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.

Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation

Report Number: WADC TR 55-12
Author: Degen, M.
Corporate Author: Brown Univ Providence RI
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-03
Pages: 110
Contract: AF 33(616)-2319
Project: 1366
Task: 70113
AD Number: AD0092966

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Lockheed Martin Missiles & Fire Control
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