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

Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds

Author(s): B. M. Leadon, G. E. Anderson
Corporate Author: Dept. Of Aeronautical Engineering, University Of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-10
Report Number: WADC TR 53-490
full text unavailable

Temp-Tapes: Improved Design, Construction, And Calibration

Author(s): Alphonso Ambrosio; Bertram Busseli
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): Ambrose B. Nutt
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): Claude R. Woodard
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-207
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A Method For The Approximate Solution Of The Heat Equation

Author(s): Jerome H. Weiner
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): Bruno A.Boley And Jerome H.Weiner
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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Indicial Downwash And Its Structural Effect On The Horizontal Tail

Author(s): Norman P. Hobbs
Corporate Author: Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report Number: WADC TR 56-164
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Improving Fatigue Life Of Fromed Stainless Steel Hydraulic Tubing By Prestressing

Author(s): C. S. Yen, B. V. Whiteson
Corporate Author: 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, Hideo
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-06
Report Number: WADC TR 56-444
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Investigation Of Methods For The Retention Of Air Frame Control Bearings In Structural Housings

Author(s): Abraham B. Asch
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): Given A. Brewer
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): Charles W. Galloway
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): Robert H. Kraichnan
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): Garabed Zartarian
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): Holt Ashley, Garabed Zartarian
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): Kenneth A. Foss, Warren L. McCabe
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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Coiled Stainless Steel Tubing: Part I. Test Results

Author(s): Joseph J. Chmura, Jr. , Ronald D. Stouffer, Albert N. Winter
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): Ronald A Stouffer, James T. Hudson, Louis F. Freitag
Corporate Author: Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1957-12
Report Number: WADC TR 57-507 Part II
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Study Of Coiled Tubing For Aircraft Hydraulic Systems

Author(s): Conrad H. Cooke; Ronald D. Stouffer
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-02
Report Number: WADC TR 55-121
full text unavailable