Solution Of The Potential Equation For The Unsteady Flow About A Triangular wing with Subsonic Leading Edges In A Supersonic Main Stream

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Report Number: WADC TR 57-258
Author(s): Luke, Yudell L., Coombs, Geraldine V., Wagner, Frank
Corporate Author(s): Midwest Research Institute
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1957-12
Pages: 38
Contract: AF 33(616)-3058
DoD Project: 7-(8-1370)
DoD Task: 70411
PB Number: PB131851
Identifier: AD0118241

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Provenance: Bombardier/Aero

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