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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10 reports

Further Studies on High-Speed Unsteady Flow

Author(s): Garabed Zartanian; Harry Sauerwein
Corporate Author: Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-09
Report Number: ASD TDR 62-463
full text by request

Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil

Author(s): J. Ray Ruetenik; Walter Herrmann
Corporate Author: Massachusetts institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-219
full text by request

Thermo-Structural Analysis Manual

Author(s): M. J. Forray; M. Newman; H. Switzky
Corporate Author: Republic Aviation Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: WADD TR 60-517 Vol II
full text by request

Prediction Of Creep Effects In Aircraft Structures

Author(s): C. W. Alesch, B. Klein, and W. Robe
Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: WADD TR 60-411 Part 2
full text by request

Methods For Analyzing Flight Vehicles During The Taxi Condition

Author(s): Theisen, J. G
Corporate Author: Lockheed Aircraft Corp Marietta GA
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-01
Report Number: ASD TR 61-177
full text by request

Strength, Efficiency, and Design Data for Beryllium Structures

Author(s): Robert F. Crawford and A. Bruce Burns
Corporate Author: Lockheed Missiles & Space Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-692
full text by request

Survey and Evaluation of Sonic Fatigue Testing Facilities

Author(s): Ralph A. Bianchi, Ronald T. Bradshaw, James H. Farrell and F. Everett Reed
Corporate Author: CONESCO Consultants in Engineering Science
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: ASD TR 61-185
full text by request

Research on Techniques of Establishing Random Type Fatigue Curves for Broad Band Sonic Loading

Author(s): J. R. Fuller
Corporate Author: The Boeing Company, Transport Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-501
full text by request

Inspection Periods Determined from Data of Crack Development and Strength Reduction of an Aircraft Structure Using Static Analysis

Author(s): Sigge Eggwertz
Corporate Author: The Aeronautical Research Institute of Sweden (FFA)
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-05
Report Number: ASD TDR 62-391
full text by request

Establishment of the Approach to, and Development of, Interim Design Criteria for Sonic Fatigue

Author(s): G. E. Fitch, T. R. Dutko, L. M. Brennan, A. G. Tipton, P. M. Belcher, P. Wang and P. A. Clawson
Corporate Author: North American Aviation, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-06
Report Number: ASD TDR 62-26
AD Number: AD0284597
full text by request