NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Bluntness and boundary-layer displacement effects on hypersonic inlet flowfields.Bluntness and boundary layer displacement effects on air breathing engine hypersonic inlet flow fields
Document ID
19660061819
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Benson, J. L.
Maslowe, S. A.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-617
Report Number: AIAA PAPER 65-617
Accession Number
66A41109
Distribution Limits
Public
Copyright
Other
Keywords
INLET FLOW
BLUNT BODY
FLOW FIELD
HYPERSONIC BOUNDARY LAYER
AIR BREATHING ENGINE

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available