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.

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2 reports

Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces

Author(s): Asher, Gifford W.
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report Number: WADC TR 54-113 Part 3
full text available

Transonic Flutter Characteristics Of A 45 Degree Swept Back All Movable Stabilizer

Author(s): D'Ewart, Benjamin B., Jr.
Corporate Author: Bell Aerospace Co Buffalo Ny
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report Number: WADC TR 57-392
full text available