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
Static aerodynamic characteristics of a rocket vehicle with thick wedge fins and sweptback leading and trailing edgesStatic aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback leading and trailing edges - supersonic wind tunnel testing of vehicle longitudinal stability
Document ID
19660004864
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Yuska, J. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3182
Report Number: NASA-TN-D-3182
Accession Number
66N14153
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET VEHICLE
AERODYNAMIC STABILITY
LONGITUDINAL STABILITY AND CONTROL
SUPERSONIC WIND TUNNEL
TRAILING EDGE
STATIC AERODYNAMIC CHARACTERISTICS

Related Records

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