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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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