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.

The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges

Report Number: WADC TR 54-196
Author: Epstein, Melvin
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Pages: 41
Contract: Laboratory Research - No Contract
Project: None Given
AD Number: AD0037709

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Lockheed Martin Missiles & Fire Control
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