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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11 reports

Optimum Re-entry Into The Earth's Atmosphere By Use Of A Variable Contol Force

Author(s): Marshall, Francis J.
Corporate Author: The University Of Chicago Institute For System Research
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-10
Report Number: WADC TR 59-515
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Digital Computation Techniques For Fluid Flow Fields With Shock

Author(s): Marshall, Francis J.
Corporate Author: The University Of Chicago Institute For System Research
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-10
Report Number: WADC TR 59-535
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Research On Rotating Stall In Axial Flow Compressors. Part III: Experiments On Laminar Seperation From A Moving wall

Author(s): Vidal, Robert J.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report Number: WADC TR 59-75 Part 3
full text unavailable

Determining Air Reactions On Moving Vehicles. Part III. Methods Of Hydrodynamics

Author(s): Krzywoblocki, M. Z.
Corporate Author: Institute For System Research, Laboratories For applied Sciences, The University Of Chicago
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-07
Report Number: WADC TR 56-51 Part 3
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The Combined Non-linear Effects Of Earth Oblateness And Atmospheric Drag On A Near-Earth Satellite

Author(s): Jaramillo, Trinidad J.
Corporate Author: The University Of Chicago Institute For System Research
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-10
Report Number: WADC TR 59-513
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Research On Rotating Stall In Axial Flow Compressors. Part IV: A Preliminary Study Of Three-dimensional Rotating Stall

Author(s): Moore, F. K.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report Number: WADC TR 59-75 Part 4
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Factors Controlling Resistance To Deformation And Mechanical Failure In Polycrystalline (Glass-Free) Ceramics

Author(s): Tefft, Wayne E.
Corporate Author: National Bureau of Standards
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-05
Report Number: WADC TR 59-278
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Detonation Induction Distances In Combustible Gaseous Mixtures At Atmospheric And Elevated Intial Pressures. IV. Hydrogen-nitric-oxide. V. Hydrogen-oxygen-diluent. VI. Theoretical Analysis

Author(s): Bollinger, Loren E.
Corporate Author: The Ohio State University Research Foundation
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-08
Report Number: WADC TR 58-591 Part 2
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Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber

Author(s): Hartunian, R. A.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report Number: WADC TR 59-75 Part 1
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Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer

Author(s): Hartunian, R. A.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report Number: WADC TR 59-75 Part 2
full text unavailable

Singular Differential Boundary Problems Of A Fourier Type

Author(s): McKelvey, Robert W.
Corporate Author: P.E.C. Corporation
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-04
Report Number: WADC TR 59-288
full text unavailable