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Subject: "Mathematics."
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Langley Research Center
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Sterling Memorial Library
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Mathematical models

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1.
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
Author
Barnwell, Richard W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:81850
Library Shelving Facility (LSF) >> NASA TM-81850
Format
Books / Microforms