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

Investigation Of Escape Capsule Systems For Multi-place Aircraft . Part I: Preliminary Investigation

Author(s): J. J. Vorachek; F. Milhoan
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: WADC TR 57-329 Part 1
full text by request

Investigation Of Escape Capsule Systems For Multi-place Aircraft. Part II: Preliminary Design And wind Tunnel Testing Of An Individual Escape Capsule

Author(s): F. M. Milhoan; J. J. Vorachek; J. D'Allura
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: WADC TR 57-329 Part 2
full text by request

Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part I: Equipment

Author(s): D. F. Turner, R. S. Brown, W. E. Snyder
Corporate Author: Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-02
Report Number: WADD TR 60-470 Part 1
full text by request

Feasibility To Determine Practicability Of Providing Mockup Improvements

Author(s): W. F. Lowe, C. C. Calvin, L. E. Doughty
Corporate Author: Chance Vought Aircraft, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report Number: WADD TR 60-579
full text by request

Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results

Author(s): Gifford W, Asher And Roy K. Watanabe
Corporate Author: Boeing Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-07
Report Number: WADD TR 61-31 Part 1
full text by request

Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials


Corporate Author: Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-10
Report Number: WADD TR 60-470 Part 2
full text by request

Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations

Author(s): Zartarian, Garabed; Tan Hsu,Pao
Corporate Author: Massachusetts Inst Of Tech Cambridge Aeroelastic And Structures Research Lab
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-04
Report Number: ASD TR 61-7
full text by request

Structural Response Of Beryllium Sheet Produced By Three Fabrication Methods

Author(s): Giemza, C. J.
Corporate Author: Martin Co Baltimore Md
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: ASD TR 61-87
full text by request

Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered

Author(s): Buck,Melving L.
Corporate Author: Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report Number: ASD TR 61-107
full text by request