Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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19 reports

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
full text unavailable

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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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
full text unavailable