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

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

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

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

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

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

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

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

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

Evaluation Of High Temperature Hydraulic Seals

Author(s): Webster, Edward A.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-01
Report Number: WADC TR 55-120

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

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

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

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

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

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

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

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

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