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Evaluation Of High Temperature Hydraulic Seals To Temperature Of 550 Degrees F. Part I: Mechanical Evealuation
Author(s): Galloway, Charles W.
Corporate Author(s): Santa Monica Division, Douglas Aircraft Company, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1958-02
Report number: WADC TR 57-76 Part 1
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Supersonic Flutter Trends As Revealed By Piston Theory Calculations
Author(s): Ashley, Holt, Zartarian, Garabed
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 58-74
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Gust Loading Of Rigid And Flexible Aircraft In Continous Atmospheric Turbulence
Author(s): Foss, Kenneth A., McCabe, Warren L.
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 57-704
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Thermal Response Of A Thin Plate With Radiation Losses
Author(s): Ambrosio, Alphonso, Ishimoto, Takao
Corporate Author(s): Dept. Of Engineering, University of California
Laboratory: Aircraft Laboratory
Date of Publication: 1958-06
Report number: WADC TR 56-212
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Basic Concepts Of The Thermodynamics Of Continuous Media
Author(s): Weiner, Jerome H., Boley, Bruno A.
Corporate Author(s): Institute of Flight Structures; Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1958-04
Report number: WADC TR 57-288
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Summary Report Of Thermal Response Studies
Author(s): Ishimoto, Takao
Corporate Author(s): University of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1958-06
Report number: WADC TR 57-373

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