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Flow with M/infinity/equals 1 past thin airfoilsPressure distribution on thin nonlifting airfoils in steady two dimensional flow with freestream Mach number at or near unity
Document ID
19700068467
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Spreiter, J. R.
Stahara, S. S.
Date Acquired
August 5, 2013
Publication Date
October 1, 1970
Subject Category
Aerodynamics
Accession Number
70A44583
Funding Number(s)
CONTRACT_GRANT: NAS2-5410
Distribution Limits
Public
Copyright
Other

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