NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter AirplaneFlight test to determine flying qualities and dynamic stability derivatives of supersonic fighter aircraft
Document ID
19660024788
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Champine, R. A. (NASA Langley Research Center Hampton, VA, United States)
Kraft, C. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Mc Laughlin, M. D. (NASA Langley Research Center Hampton, VA, United States)
White, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-10-7-58L
Report Number: NASA-MEMO-10-7-58L
Accession Number
66N34078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DYNAMIC STABILITY
FLIGHT TEST
SUPERSONIC AIRCRAFT
FLYING QUALITY
FIGHTER AIRCRAFT

Related Records

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