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Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wingPressure measurements in flight over conically cambered delta wing of F-102A aircraft at transonic speeds
Document ID
19650003087
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Keener, E. R. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-48
Accession Number
65N12688
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
CONICAL CAMBER
TRANSONIC SPEED
PRESSURE MEASUREMENT

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