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Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method
Author(s): Lee, Robert C. K., Witmer, Emmett A., Ruetenik, J . RayCorporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report number: WADC TR 54-383 Part 1
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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Boley, Bruno A., Mechanic, HaroldCorporate Author(s): Institute Of Air Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-425
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Thermo-Elastic Stresses And Deflections In Thin-Walled Beams
Author(s): Boley, Bruno A., Tolins, Irwin S.Corporate Author(s): Institute Of Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-12
Report number: WADC TR 54-426
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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, Ishimoto, TakaoCorporate Author(s): University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-01
Report number: WADC TR 54-579 Volume 3
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume IV Heat-Transfer Coefficients For Speeds Up To M-3, With Emphasis On Effects Of Wall-Temperature Variations
Author(s): Knuth, Eldon L., Bussell, BertramCorporate Author(s): University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1957-09
Report number: WADC TR 54-579 Volume 4
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New Standard Atmosphere: The WADC 1952 Model Atmosphere
Author(s): Williams, D. T., Nash, W. F., Bell, J. C.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-215
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Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures
Author(s): Needham, Robert A.Corporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-209
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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Ambrosio, Alphonso, Busseli, BertramCorporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-211
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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control
Author(s): De Leo, Richard V.Corporate Author(s): Rosemount Aeronautical Laboratories, University of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 52-128 Part 2
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Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Smith, Robert L. , Gessner, EugeneCorporate Author(s): Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-01
Report number: WADC TR 54-189 Volume 1
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