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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9 reports

Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces

Author(s): Asher, Gifford W.
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report Number: WADC TR 54-113 Part 3
full text available

Thermal Response Of A Thin Plate With Radiation Losses

Author(s): Ambrosio, Alphonso
Corporate Author: Dept. Of Engineering, University of California
Laboratory: Aircraft Laboratory
Date of Publication: 1958-06
Report Number: WADC TR 56-212
full text unavailable

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
full text unavailable

The Theory and Practice of Three Dimensional Minimum Time Dynamic Performance Maneuvers

Author(s): Dommasch, Daniel O.
Corporate Author: Dodco, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1958-04
Report Number: WADC TR 58-66
full text by request

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
full text unavailable

Basic Concepts Of The Thermodynamics Of Continuous Media

Author(s): Weiner, Jerome H.
Corporate Author: Institute of Flight Structures; Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1958-04
Report Number: WADC TR 57-288
full text unavailable

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
full text unavailable

Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Summary Report Of Thermal Response Studies

Author(s): Ishimoto, Takao
Corporate Author: University of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1958-06
Report Number: WADC TR 57-373
full text unavailable

Transonic Flutter Characteristics Of A 45 Degree Swept Back All Movable Stabilizer

Author(s): D'Ewart, Benjamin B., Jr.
Corporate Author: Bell Aerospace Co Buffalo Ny
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report Number: WADC TR 57-392
full text available