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The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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

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

Abstract:
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Provenance:
Bombardier/Aero
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