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Stability derivatives of triangular wings at supersonic speeds
Document ID
19930082383
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ribner, Herbert S
Malvestuto, Frank S , Jr
Date Acquired
August 16, 2013
Publication Date
May 1, 1948
Report/Patent Number
NACA-TN-1572
Report Number: NACA-TN-1572
Accession Number
93R11673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW VELOCITY, HIGH - SUPERSONIC
STABILITY
WINGS, DELTA - STABILITY
SIDESLIPPING
ROLLING, PITCHING & YAWING MOMENTS - WINGS, DELTA
THEORIES - WINGS

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