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Title
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STOL Tactical Aircraft Investigation Volume IV Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps
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Date
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1973
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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AFFDL TR 73-19 Volume 4
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Creator
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Monk, John R.
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Palmer, Patrick
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Lee, Jerry E.
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Corporate Author
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The Boeing Company
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Extent
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300
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Identifier
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AD0766641
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Access Rights
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Approved for public release; distribution unlimited
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Distribution Classification
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1
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Contract
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F33615-71-C-1757
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DoD Project
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643A
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DoD Task
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None Given
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Distribution Conflict
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No
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Abstract
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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.
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Report Availability
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Full text available
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Corporate Report Number
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D180-14411-1
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Date Issued
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1973-05
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Laboratory
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Air Force Flight Dynamics Laboratory
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Provenance
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AFRL/VACA
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Type
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report
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Format
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1 online resource
