X-Plane, by Austin Meyer

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X-Plane, by Austin Meyer

Simulating Aircraft/Helicopters/Bell 407 GTN750/Bell 407.acf

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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 PROPELLER 1:

root lo Re: OA209.afl

root hi Re: OA209.afl

tip lo Re: OA209.afl

tip hi Re: OA209.afl

Element # 0: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 1: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 2: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 3: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 4: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 5: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 6: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 7: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 8: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Element # 9: S= 0.122 sqr mtrs, MAC= 0.23 mtrs, incidence= 0.00 deg

Wing area for this wing=1.22

When joined to other wings, we have semi-length=5.33, sweep25=0.00, area=1.22, AR=46.67

After any wing-joining, our semi-length is 5.33 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our root chord is 0.23 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our tip chord is 0.23 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our leading-edge sweep is 0.00 deg. (for purposes of Delta-Wing factor determination only)

After any wing-joining, our mean aero sweep is 0.00 deg. (for purposes of Oswalds Efficiency determination only)

After any wing-joining, our aspect ratio is 46.67. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our taper ratio is 1.00. (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 0.8360

Finite-Wing & Element Build-Up for PROPELLER 2:

root lo Re: Wortmann FX-083.afl

root hi Re: Wortmann FX-083.afl

tip lo Re: Wortmann FX-083.afl

tip hi Re: Wortmann FX-083.afl

Element # 0: S= 0.009 sqr mtrs, MAC= 0.10 mtrs, incidence= 0.00 deg

Element # 1: S= 0.010 sqr mtrs, MAC= 0.12 mtrs, incidence= 0.00 deg

Element # 2: S= 0.012 sqr mtrs, MAC= 0.14 mtrs, incidence= 0.00 deg

Element # 3: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 4: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 5: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 6: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 7: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 8: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Element # 9: S= 0.013 sqr mtrs, MAC= 0.16 mtrs, incidence= 0.00 deg

Wing area for this wing=0.12

When joined to other wings, we have semi-length=0.82, sweep25=1.11, area=0.12, AR=11.06

After any wing-joining, our semi-length is 0.82 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our root chord is 0.16 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our tip chord is 0.16 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor

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