NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Investigation of Several Blunt Bodies to Determine Transonic Aerodynamic Characteristics Including Effects of Spinning and of Extendible Afterbody Flaps and Some Measurements of Unsteady Base PressuresTransonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angles of attack
Document ID
19660010441
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Di Camillo, J. R. (NASA Langley Research Center Hampton, VA, United States)
Fisher, L. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-1-21-59L
Accession Number
66N19730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REENTRY VEHICLE
AERODYNAMIC CHARACTERISTICS
BLUNT BODY

Related Records

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