X-Plane, by Austin Meyer

...

determination only)

After any wing-joining, our leading-edge sweep is 1.11 deg. (for purposes of Delta-Wing factor determination only)

After any wing-joining, our mean aero sweep is 1.11 deg. (for purposes of Oswalds Efficiency determination only)

After any wing-joining, our aspect ratio is 11.06. (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 0.9567

Finite-Wing & Element Build-Up for LEFT WING 3:

root lo Re: stab.afl

root hi Re: stab.afl

tip lo Re: stab.afl

tip hi Re: stab.afl

Element # 0: S= 0.193 sqr mtrs, MAC= 0.39 mtrs, incidence= 5.00 deg

Wing area for this wing=0.19

NOTE! I AM ADDING LEFT H STAB TO THE ROOT OF LEFT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=0.65)

When joined to other wings, we have semi-length=1.23, sweep25=16.11, area=0.65, AR=4.30

After any wing-joining, our semi-length is 1.23 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our root chord is 0.43 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our tip chord is 0.30 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our leading-edge sweep is 17.46 deg. (for purposes of Delta-Wing factor determination only)

After any wing-joining, our mean aero sweep is 16.11 deg. (for purposes of Oswalds Efficiency determination only)

After any wing-joining, our aspect ratio is 4.30. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our taper ratio is 0.71. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our washout is 7.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 12.00 deg, tip= 5.00 deg)

Oswalds efficiency is therefore 0.9900

Finite-Wing & Element Build-Up for RIGT WING 3:

root lo Re: stab.afl

root hi Re: stab.afl

tip lo Re: stab.afl

tip hi Re: stab.afl

Element # 0: S= 0.193 sqr mtrs, MAC= 0.39 mtrs, incidence= 5.00 deg

Wing area for this wing=0.19

NOTE! I AM ADDING RIGT H STAB TO THE ROOT OF RIGT WING 3 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=0.65)

When joined to other wings, we have semi-length=1.23, sweep25=16.11, area=0.65, AR=4.30

After any wing-joining, our semi-length is 1.23 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our root chord is 0.43 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our tip chord is 0.30 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our leading-edge sweep is 17.46 deg. (for purposes of Delta-Wing factor determination only)

After any wing-joining, our mean aero sweep is 16.11 deg. (for purposes of Oswalds Efficiency determination only)

After any wing-joining, our aspect ratio is 4.30. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our taper ratio is 0.71. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our washout is 7.00 deg. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only, root= 12.00 deg, tip= 5.00 deg)

Oswalds efficiency is therefore 0.9900

Finite-Wing & Element Build-Up for LEFT WING 4:

root lo Re: stab.afl

root hi Re: stab.afl

tip lo Re: stab.afl

tip hi Re: stab.afl

Element # 0: S= 0.141 sqr mtrs, MAC= 0.39 mtrs, incidence= -5.00 deg

Wing area for this wing=0.14

NOTE! I AM ADDING LEFT H STAB TO THE ROOT OF LEFT WING 4 (through any intermediate wings) TO FORM ONE CONTINUOUS WING! (side_S=0.60)

When joined to other wings, we have semi-length=1.15, sweep25=10.70, area=0.60, AR=4.28

After any wing-joining, our semi-length is 1.15 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our root chord is 0.43 mtrs. (for purposes of Oswalds Efficiency and Delta-Wing factor determination only)

After any wing-joining, our tip chord is