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
Some Aerodynamic and Control Studies of Lifting Reentry Configurations at Angles of Attack Up to 90 Deg at a Mach Number Of 2.91Aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90-deg at supersonic speeds
Document ID
19630004027
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clark, F. L. (NASA Langley Research Center Hampton, VA, United States)
Evans, J. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1960
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-338
Report Number: NASA-TM-X-338
Accession Number
63N13903
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC STABILITY
STABILITY AND CONTROL
LIFTING REENTRY

Related Records

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