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
Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplaneTransonic aerodynamic stability and damping in yaw and pitch for variable sweep supersonic transport model
Document ID
19660010231
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Averett, B. T. (NASA Langley Research Center Hampton, VA, United States)
Wright, B. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1207
Report Number: NASA-TM-X-1207
Accession Number
66N19520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSONIC SPEED
SUPERSONIC TRANSPORT
AERODYNAMIC STABILITY
VARIABLE SWEEP
DAMPING

Related Records

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