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The stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Document ID
19930082119
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ribner, Herbert S
Date Acquired
August 16, 2013
Publication Date
September 1, 1947
Report/Patent Number
NACA-TN-1423
Report Number: NACA-TN-1423
Accession Number
93R11409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS - DIHEDRAL
INTERFERENCE - WINGS & FUSELAGES
STABILITY CALCULATIONS
AIR FLOW VELOCITY, HIGH - SUBSONIC
AIR FLOW VELOCITY, HIGH - SUPERSONIC
WINGS, DELTA
AIRFOILS - ASPECT RATIO, SMALL
AIRFOILS, THIN
PRESSURE DISTRIBUTION - WINGS, DELTA
SIDESLIPPING

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