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19 items
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Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Author(s): Dukes, W. H., Schnitt, A.Corporate Author(s): Bell Aircraft
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part 2
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Flutter Tests of Large Straight Wing Models at High Subsonic Speeds
Author(s): White, Richard P., Jr.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 55-334
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Fabrication and Testing of Full Scale Polyester Canopies
Author(s): Harley, Robert E., Frownfelter, Charles R., Burkley, Ralph A.Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report number: WADC TR 55-259
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Soundproofing Materials and the Installation Thereof in Aircraft
Author(s): Grafman, A. J.Corporate Author(s): Frank Mayer Engineering Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 55-97
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Development of a One-Piece Plastic Windshield for High-Speed Aircraft
Author(s): Huff, Rolland D., Patrick, Stanley C., Frownfelter, Charles R.Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report number: WADC TN 55-241 Part I
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Structural Design for Aerodynamic Heating Part III. Structural Design
Author(s): Dukes, W. H., Schintt, A.Corporate Author(s): Bell Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part III
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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(s): California U.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 55-192 Volume 2
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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., Ambrosio, A., Ishimoto, TCorporate Author(s): University of California, Los Angeles, Department of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-04
Report number: WADC TR 55-192 Volume 1
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Study Of Coiled Tubing For Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Stouffer, Ronald D.Corporate Author(s): Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-02
Report number: WADC TR 55-121
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- Dukes, W. H. (3)
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