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Quiet Clean Short-haul Experimental Engine (QCSEE) under-the-wing engine simulation reportHybrid computer simulations of the under-the-wing engine were constructed to develop the dynamic design of the controls. The engine and control system includes a variable pitch fan and a digital electronic control. Simulation results for throttle bursts from 62 to 100 percent net thrust predict that the engine will accelerate 62 to 95 percent net thrust in one second.
Document ID
19800006832
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
July 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-134914
R75AEG444
Report Number: NASA-CR-134914
Report Number: R75AEG444
Accession Number
80N15091
Funding Number(s)
CONTRACT_GRANT: NAS3-18021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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