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The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Author(s): Epstein, Melvin
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report number: WADC TR 54-196
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Coefficient of Friction of Aircraft Tires on Concrete Runways
Author(s): Luthman, Robert R.
Corporate Author(s): University of Dayton
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 55-179
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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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Flutter Model Tests Of A Swept-back, All-moving Horizontal Tail At Supersonic Speeds
Author(s): Asher, Gifford W.
Corporate Author(s): Massachusetts Inst Of Tech Cambridge
Laboratory: Aircraft Laboratory
Date of Publication: 1957-11
Report number: WADC TR 56-285
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Transonic Flutter Characteristics Of A 45 Degree Swept Back All Movable Stabilizer
Author(s): D'Ewart, Benjamin B., Jr., Farrell, Robert F.
Corporate Author(s): Bell Aerospace Co Buffalo Ny
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 57-392
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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, T
Corporate 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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