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An Approximate Method of Calculating Pressures in the Tip Region of a Rectangular Wing of Circular-Arc Section at Supersonic SpeedsNo abstract available
Document ID
19930082858
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Czarnecki, Kazimierz Roman
Mueller, James N
Date Acquired
August 16, 2013
Publication Date
October 1, 1950
Subject Category
Aerodynamics
Report/Patent Number
NACA-TN-2211
Report Number: NACA-TN-2211
Accession Number
93R12148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION - WING TIPS
PRESSURE DISTRIBUTION - WINGS, RECTANGULAR
AIRFOILS, CIRCULAR - ARC
THEORIES - FLOW, LINEAR
FLOW VELOCITY, HIGH - SUPERSONIC
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