NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Propulsion systems technologyThe selection of components, control design, simulation, and tests are examined for designing supersonic propulsion systems. Inlet-engine combination under electronic control are shown. Design and test results from the integrated control for afterburning turbofan and supersonic cruise inlet are presented.
Document ID
19750023007
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hiller, K. W. (NASA Lewis Research Center Cleveland, OH, United States)
Batterton, P. G. (NASA Lewis Research Center Cleveland, OH, United States)
Burstadt, P. L. (NASA Lewis Research Center Cleveland, OH, United States)
Szuch, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Aeron. Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
75N31080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19750022995Collected WorksAeronautical Propulsion
No Preview Available