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YF-12 propulsion research program and resultsThe objectives and status of the propulsion program, along with the results acquired in the various technology areas, are discussed. The instrumentation requirements for and experience with flight testing the propulsion systems at high supersonic cruise are reported. Propulsion system performance differences between wind tunnel and flight are given. The effects of high frequency flow fluctuations (transients) on the stability of the propulsion system are described, and shock position control is evaluated.
Document ID
19770011073
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Albers, J. A. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Olinger, F. V. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Proc. of the SCAR Conf., Part 1
Subject Category
Aircraft Propulsion And Power
Accession Number
77N18017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19770011052Collected WorksProceedings of the SCAR Conference, Part 1
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