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19 items
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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 Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-207
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Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): Leadon, B. M. , Anderson, G. E.Corporate Author(s): Dept. Of Aeronautical Engineering, University Of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-10
Report number: WADC TR 53-490
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A Method For The Approximate Solution Of The Heat Equation
Author(s): Weiner, Jerome H.Corporate Author(s): Institute Of Flight Structures,Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-427
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Thermal Stress Analysis For Aircraft Structures Part II. Bibliography
Author(s): Boley, Bruno A., Weiner, Jerome H.Corporate Author(s): 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
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Improving Fatigue Life Of Fromed Stainless Steel Hydraulic Tubing By Prestressing
Author(s): Yen, C. S., Whiteson, B. V.Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1956-05
Report number: WADC TR 56-120
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On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, HideoCorporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-444
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Indicial Downwash And Its Structural Effect On The Horizontal Tail
Author(s): Hobbs, Norman P.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report number: WADC TR 56-164
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Noise Transmission from Boundary Layer Pressure Fluctuations
Author(s): Kraichnan, Robert H.Corporate Author(s): Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1956-03
Report number: WADC TN 56-263
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Coiled Stainless Steel Tubing: Part I. Test Results
Author(s): Chmura, Joseph J., Jr., Stouffer, Ronald D., Winter, Albert N.Corporate Author(s): Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1957-07
Report number: WADC TR 57-507 Part I
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