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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.

Subsonic Flutter Model Tests of Wings Carrying Heavy Tip Pods. Part 2. Swept Wings

Report Number: WADC TR 53-161 Part 2
Author(s): W. G. Brady; H. G. Maier; Walter T. Pargoff
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Pages: 104
AD Number: AD0055205

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