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.

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7 reports

Thermal Stress Analysis For Aircraft Structures Part II. Bibliography

Author(s): Boley, Bruno A.
Corporate Author: Institute Of Flight Structures, Department Of Civil Engineering and Engineering Mechanics, Columbia University.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-11
Report Number: WADC TR 56-102 Part 2
full text unavailable

Thermal Stress Analysis For Aircraft Structures Theory And Methods Of Analysis

Author(s): Boley, Bruno A.
Corporate Author: Institute Of Flight Structures, Columbia University.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Report Number: WADC TR 56-102 Part 1
full text unavailable

Study Of Coiled Tubing For Aircraft Hydraulic Systems

Author(s): Cooke, Conrad H.
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-02
Report Number: WADC TR 55-121
full text unavailable

Destruction Tests Of Aircraft Structural Components; Part 2. Development Of A Single-Channel Bending Moment Measurement Method Applicable To A Complex Built-Up Structure For Both The Elastic And The Post-Buckling Regime Of Structural Response

Author(s): Criscione, Emanuel S.
Corporate Author: Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-09
Report Number: WADC TR 54-385 Part 2
full text unavailable

A Method For The Approximate Solution Of The Heat Equation

Author(s): Weiner, Jerome H.
Corporate Author: Institute Of Flight Structures,Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report Number: WADC TR 54-427
full text unavailable

Development of a One-Piece Plastic Windshield for High-Speed Aircraft

Author(s): Huff, Rolland D.
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report Number: WADC TN 55-241 Part I
full text unavailable

Structural Design for Aerodynamic Heating Part III. Structural Design

Author(s): Dukes, W. H.
Corporate Author: Bell Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report Number: WADC TR 55-305 Part III
full text unavailable