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Low-speed aerodynamics of the upper-surface blown jet flapReview of the results of recent wind-tunnel investigations conducted to provide fundamental aerodynamic information on the upper-surface blown jet-flap concept incorporating high-bypass-ratio turbofan engines. The results of the investigations have shown the concept to have aerodynamic performance generally comparable to that of other externally blown high-lift systems. Some of the more critical problem areas associated with this concept are covered, and solutions which have been found for these problems are discussed.
Document ID
19740052230
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, J. L., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Phelps, A. E., III
(U.S. Army, Air Mobility Research and Development Laboratory, Hampton Va., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
SAE PAPER 740470
Meeting Information
Meeting: Air Transportation Meeting
Location: Dallas, TX
Start Date: April 30, 1974
End Date: May 2, 1974
Sponsors: Society of Automotive Engineers
Accession Number
74A34980
Distribution Limits
Public
Copyright
Other

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