STOL Tactical Aircraft Investigation Volume IV Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps

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Report Number: AFFDL TR 73-19 Volume 4
Author(s): Monk, John R., Palmer, Patrick, Lee, Jerry E.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Corporate Report Number: D180-14411-1
Date of Publication: 1973-05
Pages: 300
Contract: F33615-71-C-1757
DoD Project: 643A
Identifier: AD0766641

The report presents the analysis of 728 hours of testing, conducted in the Boeing V/STOL 20 x 20 ft. Wind Tunnel, on a model of a medium STOL transport with vectored thrust and jet flap powered-lift systems. The interactions between the two powered lift systems and the basic airplane aerodynamics are presented for a systematic series of configuration changes which include sweep and nacelle location.

Provenance: AFRL/VACA

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