The 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.
Recent propulsion system flight tests at the NASA Dryden Flight Research Center
Flight Testing Conference ; 1981 ; Las Vegas, NV
1981-11-01
Conference paper
No indication
English
NASA Dryden Flight Research Center
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