19 reports
Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): Leadon, B. M. Corporate Author: 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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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Ambrosio, Alphonso Corporate Author: University Of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-211
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Principles of Canopy Design For Military Aircraft
Author(s): Nutt, Ambrose B. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1953-04 Report Number: WADC TR 53-92
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An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-207
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Study Of Coiled Tubing For Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H. Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1955-02 Report Number: WADC TR 55-121
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A Method For The Approximate Solution Of The Heat Equation
Author(s): Weiner, Jerome H. Corporate Author: 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. Corporate Author: 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. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1956-05 Report Number: WADC TR 56-120
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Indicial Downwash And Its Structural Effect On The Horizontal Tail
Author(s): Hobbs, Norman P. Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-08 Report Number: WADC TR 56-164
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On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, Hideo Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1956-06 Report Number: WADC TR 56-444
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Coiled Stainless Steel Tubing: Part I. Test Results
Author(s): Chmura, Joseph J., Jr. Corporate Author: Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1957-07 Report Number: WADC TR 57-507 Part I
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Coiled Stainless Steel Tubing: Part II, Design Manual
Author(s): Stouffer, Ronald A. Corporate Author: Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-507 Part II
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Investigation Of Methods For The Retention Of Air Frame Control Bearings In Structural Housings
Author(s): Asch, Abraham B. Corporate Author: Asch Equipment Company Laboratory: Aircraft Laboratory Date of Publication: 1957-01 Report Number: WADC TR 56-502
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Synthetic Mica High Temperature Strain Gage Research
Author(s): Brewer, Given A. Corporate Author: Brewer Engineering Laboratories Laboratory: Aircraft Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-306
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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: 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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Noise Transmission from Boundary Layer Pressure Fluctuations
Author(s): Kraichnan, Robert H. Corporate Author: Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1956-03 Report Number: WADC TN 56-263
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Unsteady Airloads On Pointed Airfoils And Slender Bodies At High Mach Numbers
Author(s): Zartarian, Garabed Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1959-12 Report Number: WADC TR 59-583
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Supersonic Flutter Trends As Revealed By Piston Theory Calculations
Author(s): Ashley, Holt Corporate Author: 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. Corporate Author: 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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