Contrails
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.

Limit your search

Publication Date
Laboratory

106 reports

Coiled Stainless Steel Tubing: Part I. Test Results

Author(s): Chmura, Joseph J., Jr.
Corporate Author: Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1957-07
Report Number: WADC TR 57-507 Part I
full text unavailable

Flutter Tests of Large Straight Wing Models at High Subsonic Speeds

Author(s): White, Richard P., Jr.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report Number: WADC TR 55-334
full text available

Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques

Author(s): McCarthy, John F., Jr.
Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report Number: WADC TR 54-113 Part 1
full text available

Studies on Thermal Stresses for Aircraft Structures Exposed to Transient External Heating. Volume I. Evaluation of the Thermal Response, Force and Moment in a Plate.

Author(s): Mahlmeister, J. E.
Corporate Author: University of California, Los Angeles, Department of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-04
Report Number: WADC TR 55-192 Volume 1
full text available

Studies On Thermal Stresses For Aircraft Structures Exposed To Transient External Heating, Volume II. An Analytical Method For The Prediction Of Behavior Of A Sheet-Stringer Panel With A Uniformly Heated Surface

Author(s): Mahlmeister, J. E.
Corporate Author: California U.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report Number: WADC TR 55-192 Volume 2
full text available

Aerodynamic Shape of the Wing Tips

Author(s): Hoerner, Sighard
Laboratory: Aircraft Laboratory
Report Number: AF TR 5752
full text available