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speedrestriction
29th Mar 2020, 11:58
Could anyone explain to me the reason why the wing span at the leading edge of the F-15 wing is greater than the trailing edge. I appreciate that many fighter aircraft of the 70s-00s were designed to incorporate wing tip mounted hardpoints which obviously constrains the wing design options. Does the F-15’s wingtip imbue any particular aerodynamic improvements?

JohnFTEng
29th Mar 2020, 13:02
IIRC they got the lift distribution wrong at design stage and only found it at early flight test. Quick solution was to reduce TE torque by cutting back outboard area. This from memories reAding Flight International at uni in late 60s / early 70s

itsnotthatbloodyhard
29th Mar 2020, 13:11
Here you go: http://aviationarchives.net/The%20Saga%20of%20the%20F-15%20Wing%20Tips_Revised%201_.pdf

(TLDR: to alleviate buffet due to shock-induced separation)

speedrestriction
29th Mar 2020, 14:09
Thank you both very much. Far more interesting story than I had guessed.

Capn Bloggs
30th Mar 2020, 11:43
Fascinating. "Told ya so!"; Jack would've been smiling.

B2N2
30th Mar 2020, 12:30
Great story thanks !

turbidus
1st Apr 2020, 12:18
more fun reading...

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890009868.pdf

RVF750
1st Apr 2020, 16:56
Also this is a nice one.

https://www.youtube.com/watch?v=9UGaYQybb4E