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Recent propulsion system flight tests at the NASA Dryden Flight Research CenterThe article presents a summary of the propulsion system tests conducted on a number of aircraft at the NASA Dryden Flight Research Center. The tests included digital engine control systems, engine-inlet compatibility, inlet-airframe interactions, nozzle-boattail drag and advanced turboprop acoustics. Among the aircraft evaluated were the F-15, HiMAT, F-14, and the JetStar.
Document ID
19820030339
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burcham, F. W., Jr. (NASA Flight Research Center Edwards, CA, United States)
Myers, L. P. (NASA Flight Research Center Edwards, CA, United States)
Nugent, J. (NASA Flight Research Center Edwards, CA, United States)
Lasagna, P. L. (NASA Flight Research Center Edwards, CA, United States)
Webb, L. D. (NASA Flight Research Center Edwards AFB, CA, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 81-2438
Meeting Information
Meeting: Flight Testing Conference
Location: Las Vegas, NV
Start Date: November 11, 1981
End Date: November 13, 1981
Accession Number
82A13874
Distribution Limits
Public
Copyright
Other

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