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Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engineThe investigation utilizing a small turbofan engine was conducted to evaluate static turning performance and pressure and temperature environment of an upper surface blown wing and flap segment. The tests involved modifications of the engine primary nozzle to alleviate high-temperature problems on the wing and flaps without adversely affecting static turning performance over the desired range of flap deflection and thrust condition.
Document ID
19750008432
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Shivers, J. P. (NASA Langley Research Center Hampton, VA, United States)
Smith, C. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TN-D-7816
L-9712
Report Number: NASA-TN-D-7816
Report Number: L-9712
Accession Number
75N16504
Funding Number(s)
PROJECT: RTOP 760-61-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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