STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings

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Report Number: AFFDL TR 73-19 Volume 2 Part 2
Author(s): Davenport, Franklyn J.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-06
Pages: 118
Contract: F33615-71-C-1757
DoD Project: 643A
Identifier: AD0766877

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Provenance: AFRL/VACA

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