•••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• X-Plane, by Austin Meyer Simulating Aircraft/X-Aviation/IXEG 737 Classic/B733.acf •••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• x location positive aft x force positive right pitch/alpha pos nose up y location positive right y force positive up roll pos right z location positive up z force positive aft yaw/beta pos nose right elevator, aileron, spoiler positive control surface up rudder positive control surface right drag-yaw positive control surface deployed pitch cyclic prop pitch positive request nose up roll cyclic prop pitch positive request nose right Finite-Wing & Element Build-Up for LEFT WING 1: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 4.709 sqr mtrs, MAC= 7.48 mtrs, incidence= 0.00 deg Element # 1: S= 4.414 sqr mtrs, MAC= 7.01 mtrs, incidence= 0.00 deg Element # 2: S= 4.118 sqr mtrs, MAC= 6.54 mtrs, incidence= 1.80 deg Element # 3: S= 3.823 sqr mtrs, MAC= 6.07 mtrs, incidence= 1.80 deg Element # 4: S= 3.527 sqr mtrs, MAC= 5.60 mtrs, incidence= 1.70 deg Element # 5: S= 3.232 sqr mtrs, MAC= 5.14 mtrs, incidence= 1.60 deg Element # 6: S= 2.937 sqr mtrs, MAC= 4.67 mtrs, incidence= 1.50 deg Element # 7: S= 2.641 sqr mtrs, MAC= 4.20 mtrs, incidence= 1.40 deg Wing area for this wing=29.40 NOTE! I AM ADDING LEFT WING 2 TO THE TIP OF LEFT WING 1 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=54.80) NOTE! I AM ADDING LEFT WING 3 TO THE TIP OF LEFT WING 1 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for RIGT WING 1: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 4.709 sqr mtrs, MAC= 7.48 mtrs, incidence= 0.00 deg Element # 1: S= 4.414 sqr mtrs, MAC= 7.01 mtrs, incidence= 0.00 deg Element # 2: S= 4.118 sqr mtrs, MAC= 6.54 mtrs, incidence= 1.80 deg Element # 3: S= 3.823 sqr mtrs, MAC= 6.07 mtrs, incidence= 1.80 deg Element # 4: S= 3.527 sqr mtrs, MAC= 5.60 mtrs, incidence= 1.70 deg Element # 5: S= 3.232 sqr mtrs, MAC= 5.14 mtrs, incidence= 1.60 deg Element # 6: S= 2.937 sqr mtrs, MAC= 4.67 mtrs, incidence= 1.50 deg Element # 7: S= 2.641 sqr mtrs, MAC= 4.20 mtrs, incidence= 1.40 deg Wing area for this wing=29.40 NOTE! I AM ADDING RIGT WING 2 TO THE TIP OF RIGT WING 1 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=54.80) NOTE! I AM ADDING RIGT WING 3 TO THE TIP OF RIGT WING 1 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for LEFT WING 2: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 4.368 sqr mtrs, MAC= 3.81 mtrs, incidence= 1.40 deg Element # 1: S= 4.027 sqr mtrs, MAC= 3.52 mtrs, incidence= 1.30 deg Element # 2: S= 3.686 sqr mtrs, MAC= 3.22 mtrs, incidence= 1.20 deg Element # 3: S= 3.345 sqr mtrs, MAC= 2.92 mtrs, incidence= 1.10 deg Element # 4: S= 3.004 sqr mtrs, MAC= 2.62 mtrs, incidence= 1.00 deg Element # 5: S= 2.663 sqr mtrs, MAC= 2.33 mtrs, incidence= 0.90 deg Element # 6: S= 2.322 sqr mtrs, MAC= 2.03 mtrs, incidence= 0.80 deg Element # 7: S= 1.981 sqr mtrs, MAC= 1.73 mtrs, incidence= 0.70 deg Wing area for this wing=25.40 NOTE! I AM ADDING LEFT WING 1 TO THE ROOT OF LEFT WING 2 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=54.80) NOTE! I AM ADDING LEFT WING 3 TO THE TIP OF LEFT WING 2 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for RIGT WING 2: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 4.368 sqr mtrs, MAC= 3.81 mtrs, incidence= 1.40 deg Element # 1: S= 4.027 sqr mtrs, MAC= 3.52 mtrs, incidence= 1.30 deg Element # 2: S= 3.686 sqr mtrs, MAC= 3.22 mtrs, incidence= 1.20 deg Element # 3: S= 3.345 sqr mtrs, MAC= 2.92 mtrs, incidence= 1.10 deg Element # 4: S= 3.004 sqr mtrs, MAC= 2.62 mtrs, incidence= 1.00 deg Element # 5: S= 2.663 sqr mtrs, MAC= 2.33 mtrs, incidence= 0.90 deg Element # 6: S= 2.322 sqr mtrs, MAC= 2.03 mtrs, incidence= 0.80 deg Element # 7: S= 1.981 sqr mtrs, MAC= 1.73 mtrs, incidence= 0.70 deg Wing area for this wing=25.40 NOTE! I AM ADDING RIGT WING 1 TO THE ROOT OF RIGT WING 2 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=54.80) NOTE! I AM ADDING RIGT WING 3 TO THE TIP OF RIGT WING 2 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for LEFT WING 3: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 0.091 sqr mtrs, MAC= 1.51 mtrs, incidence= 0.80 deg Element # 1: S= 0.082 sqr mtrs, MAC= 1.37 mtrs, incidence= 0.80 deg Element # 2: S= 0.074 sqr mtrs, MAC= 1.22 mtrs, incidence= 0.80 deg Element # 3: S= 0.065 sqr mtrs, MAC= 1.08 mtrs, incidence= 0.80 deg Wing area for this wing=0.31 NOTE! I AM ADDING LEFT WING 2 TO THE ROOT OF LEFT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=25.71) NOTE! I AM ADDING LEFT WING 1 TO THE ROOT OF LEFT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for RIGT WING 3: root lo Re: B733 HI.afl root hi Re: B733 HI.afl tip lo Re: B733 HI.afl tip hi Re: B733 HI.afl Element # 0: S= 0.091 sqr mtrs, MAC= 1.51 mtrs, incidence= 0.80 deg Element # 1: S= 0.082 sqr mtrs, MAC= 1.37 mtrs, incidence= 0.80 deg Element # 2: S= 0.074 sqr mtrs, MAC= 1.22 mtrs, incidence= 0.80 deg Element # 3: S= 0.065 sqr mtrs, MAC= 1.08 mtrs, incidence= 0.80 deg Wing area for this wing=0.31 NOTE! I AM ADDING RIGT WING 2 TO THE ROOT OF RIGT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=25.71) NOTE! I AM ADDING RIGT WING 1 TO THE ROOT OF RIGT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=55.11) When joined to other wings, we have semi-length=16.31, sweep25=27.62, area=55.11, AR=7.58 After any wing-joining, our semi-length is 16.31 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 7.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.01 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 32.59 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 27.62 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 7.58. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.13. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is -0.80 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.80 deg) Oswalds efficiency is therefore 0.9869 Finite-Wing & Element Build-Up for LEFT H STAB: root lo Re: Hstab.afl root hi Re: Hstab.afl tip lo Re: Hstab.afl tip hi Re: Hstab.afl Element # 0: S= 2.877 sqr mtrs, MAC= 3.76 mtrs, incidence= -1.80 deg Element # 1: S= 2.612 sqr mtrs, MAC= 3.41 mtrs, incidence= -1.80 deg Element # 2: S= 2.346 sqr mtrs, MAC= 3.07 mtrs, incidence= -1.80 deg Element # 3: S= 2.081 sqr mtrs, MAC= 2.72 mtrs, incidence= -1.80 deg Element # 4: S= 1.816 sqr mtrs, MAC= 2.38 mtrs, incidence= -1.80 deg Element # 5: S= 1.550 sqr mtrs, MAC= 2.03 mtrs, incidence= -1.80 deg Element # 6: S= 1.285 sqr mtrs, MAC= 1.68 mtrs, incidence= -1.80 deg Element # 7: S= 1.019 sqr mtrs, MAC= 1.34 mtrs, incidence= -1.80 deg Wing area for this wing=15.59 When joined to other wings, we have semi-length=7.07, sweep25=30.00, area=15.59, AR=4.81 After any wing-joining, our semi-length is 7.07 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 3.93 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.16 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 34.63 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 30.00 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 4.81. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.29. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is 0.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= -1.80 deg, tip= -1.80 deg) Oswalds efficiency is therefore 0.9932 Finite-Wing & Element Build-Up for RIGT H STAB: root lo Re: Hstab.afl root hi Re: Hstab.afl tip lo Re: Hstab.afl tip hi Re: Hstab.afl Element # 0: S= 2.877 sqr mtrs, MAC= 3.76 mtrs, incidence= -1.80 deg Element # 1: S= 2.612 sqr mtrs, MAC= 3.41 mtrs, incidence= -1.80 deg Element # 2: S= 2.346 sqr mtrs, MAC= 3.07 mtrs, incidence= -1.80 deg Element # 3: S= 2.081 sqr mtrs, MAC= 2.72 mtrs, incidence= -1.80 deg Element # 4: S= 1.816 sqr mtrs, MAC= 2.38 mtrs, incidence= -1.80 deg Element # 5: S= 1.550 sqr mtrs, MAC= 2.03 mtrs, incidence= -1.80 deg Element # 6: S= 1.285 sqr mtrs, MAC= 1.68 mtrs, incidence= -1.80 deg Element # 7: S= 1.019 sqr mtrs, MAC= 1.34 mtrs, incidence= -1.80 deg Wing area for this wing=15.59 When joined to other wings, we have semi-length=7.07, sweep25=30.00, area=15.59, AR=4.81 After any wing-joining, our semi-length is 7.07 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 3.93 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.16 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 34.63 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 30.00 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 4.81. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.29. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is 0.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= -1.80 deg, tip= -1.80 deg) Oswalds efficiency is therefore 0.9932 Finite-Wing & Element Build-Up for VERT STAB 1: root lo Re: NACA 0009 (symmetrical).afl root hi Re: NACA 0009 (symmetrical).afl tip lo Re: NACA 0009 (symmetrical).afl tip hi Re: NACA 0009 (symmetrical).afl Element # 0: S= 5.873 sqr mtrs, MAC= 6.82 mtrs, incidence= 0.00 deg Element # 1: S= 3.396 sqr mtrs, MAC= 4.06 mtrs, incidence= 0.00 deg Wing area for this wing=9.27 When joined to other wings, we have semi-length=4.88, sweep25=69.00, area=9.27, AR=0.66 After any wing-joining, our semi-length is 4.88 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 8.14 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 2.47 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 73.68 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 69.00 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 0.66. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.30. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is 0.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.00 deg) Oswalds efficiency is therefore 0.9830 Finite-Wing & Element Build-Up for VERT STAB 2: root lo Re: NACA 0009 (symmetrical).afl root hi Re: NACA 0009 (symmetrical).afl tip lo Re: NACA 0009 (symmetrical).afl tip hi Re: NACA 0009 (symmetrical).afl Element # 0: S= 15.043 sqr mtrs, MAC= 4.63 mtrs, incidence= 0.00 deg Element # 1: S= 8.765 sqr mtrs, MAC= 2.77 mtrs, incidence= 0.00 deg Wing area for this wing=23.81 When joined to other wings, we have semi-length=8.05, sweep25=35.00, area=23.81, AR=3.65 After any wing-joining, our semi-length is 8.05 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our root chord is 5.52 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our tip chord is 1.71 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our leading-edge sweep is 40.19 deg. (for purposes of Delta-Wing factor determination only) After any wing-joining, our mean aero sweep is 35.00 deg. (for purposes of Oswalds Efficiency determination only) After any wing-joining, our aspect ratio is 3.65. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our taper ratio is 0.31. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only) After any wing-joining, our washout is 0.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 0.00 deg, tip= 0.00 deg) Oswalds efficiency is therefore 0.9888 Critical altitude=0.0000 mtrs, rho at crit alt=1.2250 kg/mmm, rho at SL=1.2250 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 29.401 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 58.803 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 84.199 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 109.595 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 109.906 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 110.218 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 125.804 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 141.390 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 150.659 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 174.467 square meters for all wings listed so far Now for MI from FUSELAGE: The frontal area is 10.808 square meters The side area is 106.776 square meters The top area is 94.993 square meters The longitudinal centroid is 0.18 meters The lateral centroid is 0.00 meters The vertical centroid is 1.03 meters The RUNNING TOTAL wetted area is 495.713 square meters, for the entire craft, including all wings, top and bottom surfaces, and all bodies listed so far The RUNNING TOTAL radius of gyration in roll is 3.07 meters The RUNNING TOTAL radius of gyration in pitch is 7.57 meters The RUNNING TOTAL radius of gyration in yaw is 7.79 meters Now for MI from NACELLE 1: The frontal area is 3.219 square meters The side area is 7.251 square meters The top area is 10.373 square meters The longitudinal centroid is -2.45 meters The lateral centroid is -4.95 meters The vertical centroid is -0.87 meters The RUNNING TOTAL wetted area is 529.586 square meters, for the entire craft, including all wings, top and bottom surfaces, and all bodies listed so far The RUNNING TOTAL radius of gyration in roll is 3.19 meters The RUNNING TOTAL radius of gyration in pitch is 7.36 meters The RUNNING TOTAL radius of gyration in yaw is 7.65 meters Now for MI from NACELLE 2: The frontal area is 3.219 square meters The side area is 7.252 square meters The top area is 10.373 square meters The longitudinal centroid is -2.45 meters The lateral centroid is 4.95 meters The vertical centroid is -0.87 meters The RUNNING TOTAL wetted area is 563.460 square meters, for the entire craft, including all wings, top and bottom surfaces, and all bodies listed so far The RUNNING TOTAL radius of gyration in roll is 3.38 meters The RUNNING TOTAL radius of gyration in pitch is 7.17 meters The RUNNING TOTAL radius of gyration in yaw is 7.57 meters As specified in the manual radius of gyration in the Weight and Balance screen in Plane Maker: The radius of gyration in roll is 4.27 m The radius of gyration in pitch is 12.34 m The radius of gyration in yaw is 13.50 m For LEFT WING 1: Full slat #1 deployment will cause coefficient data to spread out alpha-wise to 150.28% of original Full slat #1 deployment will also change the lift coefficient by the same amount (keeping the lift SLOPE the same) For RIGT WING 1: Full slat #1 deployment will cause coefficient data to spread out alpha-wise to 150.28% of original Full slat #1 deployment will also change the lift coefficient by the same amount (keeping the lift SLOPE the same) For LEFT WING 2: Full slat #2 deployment will cause coefficient data to spread out alpha-wise to 150.28% of original Full slat #2 deployment will also change the lift coefficient by the same amount (keeping the lift SLOPE the same) For RIGT WING 2: Full slat #2 deployment will cause coefficient data to spread out alpha-wise to 150.28% of original Full slat #2 deployment will also change the lift coefficient by the same amount (keeping the lift SLOPE the same) The centroid of wing 1->4 foils is at 3.04 m (positive aft from CG) The average chord of wing 1->4 foils is 4.73 m The static margin is 0.64 (positive stable, in mean aero chords of wings 1->4) The CG is at 30.63 % (of the mean aerodynamc chord of wings 1->4) Critical altitude=0.00 mtrs, rho at crit alt=1.23 kg/mmm, rho at SL=1.23 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 3.382 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 6.763 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 10.643 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 14.523 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 14.868 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 15.214 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 17.005 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 18.795 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 20.950 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 21.289 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 30.322 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 60.644 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 80.345 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 100.046 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 114.859 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 129.671 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 130.013 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 130.356 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 147.256 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 164.156 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 174.091 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 202.193 square meters for all wings listed so far After MISC WING 1, the RUNNING TOTAL wetted area is 204.393 square meters for all wings listed so far After MISC WING 3, the RUNNING TOTAL wetted area is 204.705 square meters for all wings listed so far After MISC WING 4, the RUNNING TOTAL wetted area is 206.904 square meters for all wings listed so far After MISC WING 6, the RUNNING TOTAL wetted area is 207.216 square meters for all wings listed so far Critical altitude=1219.200 mtrs, rho at crit alt=1.088 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.1260 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 0.202 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 0.405 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 1.391 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 2.377 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 3.844 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 101.834 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 203.669 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 300.871 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 398.074 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 435.236 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 472.398 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 474.832 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 477.266 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 528.993 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 580.720 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 588.865 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 648.418 square meters for all wings listed so far After ENG1 PYLN 1, the RUNNING TOTAL wetted area is 662.042 square meters for all wings listed so far After ENG2 PYLN 1, the RUNNING TOTAL wetted area is 675.667 square meters for all wings listed so far After ENG1 PYLN 2, the RUNNING TOTAL wetted area is 679.317 square meters for all wings listed so far After ENG2 PYLN 2, the RUNNING TOTAL wetted area is 682.968 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 101.834 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 203.669 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 300.871 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 398.074 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 435.236 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 472.398 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 474.832 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 477.266 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 528.993 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 580.720 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 588.865 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 648.418 square meters for all wings listed so far After ENG1 PYLN 1, the RUNNING TOTAL wetted area is 662.042 square meters for all wings listed so far After ENG2 PYLN 1, the RUNNING TOTAL wetted area is 675.667 square meters for all wings listed so far After ENG1 PYLN 2, the RUNNING TOTAL wetted area is 679.317 square meters for all wings listed so far After ENG2 PYLN 2, the RUNNING TOTAL wetted area is 682.968 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 3.382 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 6.763 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 10.643 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 14.523 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 14.868 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 15.214 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 17.005 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 18.795 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 20.950 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 21.289 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 101.834 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 203.669 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 300.871 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 398.074 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 435.236 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 472.398 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 474.832 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 477.266 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 528.993 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 580.720 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 588.865 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 648.418 square meters for all wings listed so far After ENG1 PYLN 1, the RUNNING TOTAL wetted area is 662.042 square meters for all wings listed so far After ENG2 PYLN 1, the RUNNING TOTAL wetted area is 675.667 square meters for all wings listed so far After ENG1 PYLN 2, the RUNNING TOTAL wetted area is 679.317 square meters for all wings listed so far After ENG2 PYLN 2, the RUNNING TOTAL wetted area is 682.968 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 20.132 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 40.263 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 44.550 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 48.836 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 49.560 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 50.284 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 53.863 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 57.443 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 62.891 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 101.834 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 203.669 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 300.871 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 398.074 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 435.236 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 472.398 square meters for all wings listed so far After LEFT WING 4, the RUNNING TOTAL wetted area is 474.832 square meters for all wings listed so far After RIGT WING 4, the RUNNING TOTAL wetted area is 477.266 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 528.993 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 580.720 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 588.865 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 648.418 square meters for all wings listed so far After ENG1 PYLN 1, the RUNNING TOTAL wetted area is 662.042 square meters for all wings listed so far After ENG2 PYLN 1, the RUNNING TOTAL wetted area is 675.667 square meters for all wings listed so far After ENG1 PYLN 2, the RUNNING TOTAL wetted area is 679.317 square meters for all wings listed so far After ENG2 PYLN 2, the RUNNING TOTAL wetted area is 682.968 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 3.382 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 6.763 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 10.643 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 14.523 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 14.868 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 15.214 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 17.005 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 18.795 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 20.950 square meters for all wings listed so far After VERT STAB 2, the RUNNING TOTAL wetted area is 21.289 square meters for all wings listed so far Critical altitude=3962.400 mtrs, rho at crit alt=0.823 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.4892 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 7.820 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 15.640 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 28.246 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 40.853 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 46.299 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 51.745 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 58.774 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 65.802 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 79.539 square meters for all wings listed so far After MISC WING 1, the RUNNING TOTAL wetted area is 79.666 square meters for all wings listed so far After MISC WING 2, the RUNNING TOTAL wetted area is 79.695 square meters for all wings listed so far After MISC WING 3, the RUNNING TOTAL wetted area is 81.842 square meters for all wings listed so far After MISC WING 4, the RUNNING TOTAL wetted area is 84.006 square meters for all wings listed so far After MISC WING 5, the RUNNING TOTAL wetted area is 84.108 square meters for all wings listed so far After MISC WING 6, the RUNNING TOTAL wetted area is 84.210 square meters for all wings listed so far Critical altitude=0.000 mtrs, rho at crit alt=1.225 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0000 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 3.153 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 6.306 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 10.627 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 14.948 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 17.040 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 19.133 square meters for all wings listed so far After VERT STAB 1, the RUNNING TOTAL wetted area is 21.530 square meters for all wings listed so far Critical altitude=914.400 mtrs, rho at crit alt=1.121 kg/mmm, rho at SL=1.225 kg/mmm, engine power boosted to 1.0927 of original After LEFT WING 1, the RUNNING TOTAL wetted area is 39.933 square meters for all wings listed so far After RIGT WING 1, the RUNNING TOTAL wetted area is 79.866 square meters for all wings listed so far After LEFT WING 2, the RUNNING TOTAL wetted area is 117.896 square meters for all wings listed so far After RIGT WING 2, the RUNNING TOTAL wetted area is 155.925 square meters for all wings listed so far After LEFT WING 3, the RUNNING TOTAL wetted area is 171.906 square meters for all wings listed so far After RIGT WING 3, the RUNNING TOTAL wetted area is 187.887 square meters for all wings listed so far After LEFT H STAB, the RUNNING TOTAL wetted area is 213.206 square meters for all wings listed so far After RIGT H STAB, the RUNNING TOTAL wetted area is 238.525 square meters fo