NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High-speed inlet research program and supporting analysisThe technology challenges faced by the high speed inlet designer are discussed by describing the considerations that went into the design of the Mach 5 research inlet. It is shown that the emerging three dimensional viscous computational fluid dynamics (CFD) flow codes, together with small scale experiments, can be used to guide larger scale full inlet systems research. Then, in turn, the results of the large scale research, if properly instrumented, can be used to validate or at least to calibrate the CFD codes.
Document ID
19920013299
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coltrin, Robert E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Aeropropulsion 1987
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N22542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available