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Two-dimensional unsteady lift problems in supersonic flight
Document ID
19930082282
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Heaslet, Max A
Lomax, Harvard
Date Acquired
August 16, 2013
Publication Date
June 1, 1948
Report/Patent Number
NACA-TN-1621
Report Number: NACA-TN-1621
Accession Number
93R11572
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW - AIRFOILS 2-DIMENSIONAL
LOADS, GUST - WINGS
LOAD DISTRIBUTION - WINGS
AIRFOILS - ANGLE OF ATTACK
AIR FLOW VELOCITY, HIGH - SUPERSONIC
THEORIES - WINGS
PRESSURE DISTRIBUTION - AIRFOILS
LIFT DISTRIBUTION - WINGS
AIR FLOW - AIRFOILS OSCILLATING
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