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

Report Availability

11 reports

Soundproofing Materials and the Installation Thereof in Aircraft

Author(s): Grafman, A. J.
Corporate Author: Frank Mayer Engineering Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report Number: WADC TR 55-97
full text available

Structural Design for Aerodynamic Heating. Part II. Analytical Studies

Author(s): Dukes, W. H.
Corporate Author: Bell Aircraft
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report Number: WADC TR 55-305 Part 2
full text available

Coefficient of Friction of Aircraft Tires on Concrete Runways

Author(s): Luthman, Robert R.
Corporate Author: University of Dayton
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report Number: WADC TR 55-179
full text available

Structural Design For Aerodynamic Heating. Part I: Design Information

Author(s): Dukes, W. H.
Corporate Author: Bell Aircraft Corpoartion
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report Number: WADC TR 55-305 Part 1
full text available

Testing Of Metal Boss Seals

Author(s): Kupiec, Harry P.
Corporate Author: Aircraft Equipment Testing Co.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-04
Report Number: WADC TR 55-163
full text available

Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume III Thermal Response Of The Skin And Support Flange Of A Structural Joint

Author(s): Ambrosio, Alphonso
Corporate Author: University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-01
Report Number: WADC TR 54-579 Volume 3
full text available

Fabrication and Testing of Full Scale Polyester Canopies

Author(s): Harley, Robert E.
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report Number: WADC TR 55-259
full text available

Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks

Author(s): McCarthy, John F., Jr.
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report Number: WADC TR 54-113 Part 2
full text available

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

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