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.

Limit your search

Publication Date

27 reports

Thermo-Structural Analysis Manual

Author(s): Switzky, H.; Forray, M.J.; Newman, M.
Corporate Author: Republic Aviation Corp Farmingdale N Y
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-08
Report Number: WADD TR 60-517 Volume 1
full text available

Study of a Sonic Load Recorder, Volume I.

Author(s): Jay H. Ball, Norman Doelling, Denis U. Noiseux, Edward A. Starr
Corporate Author: Bolt Beranek and Newman Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-11
Report Number: ASD TDR 62-165 Volume 1
full text available

Application of the NASA Kernel-Function Procedures to Generally Deforming Wings

Author(s): None Given
Corporate Author: Aerojet-General Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-409
full text available

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

Track Tests Of Canopy Escape Capsule

Author(s): Lubinski, Thomas P.
Corporate Author: Coleman Engineering Co Inc Torrance Calif
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-08
Report Number: ASD TDR 62-404
full text available

Structural Flight Loads Data from F-106A Aircraft

Author(s): Artie Vahldiek; John B. Monfort
Corporate Author: Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TDR 62-246
full text unavailable

Investigation of Stabilization and Control Systems for Application to Aero Space Vehicle Escape Capsules

Author(s): F. E. Chew; L. Oling; H. A. Clutz
Corporate Author: Chance Vought Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-06
Report Number: ASD TDR 62-243
full text unavailable

Practical Aspects of Aerothermoelastic Modelling

Author(s): M. Schlessinger; B. Omilian; J. Deutschman; J. S. Isenberg
Corporate Author: Flight Sciences Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-705
full text unavailable

Uniform Heating Effects on the Response of a High Speed Vehical to Discrete and Continuous Gusts

Author(s): R. P. Peboulet; P. G. Warner
Corporate Author: General Dynamics
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-328
full text unavailable

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

On Developing a Low Altitude Turbulence Model for Aircraft Gust Loads

Author(s): U. O. Lappe; J. Clodman
Corporate Author: New York University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-06
Report Number: ASD TDR 62-152
full text unavailable

Lift, Pitching-Moment, and Rolling-Moment Coefficients on Planar, Twisted, and Cambered Wings and Flaps for a 70 Degree Delta Wing: Part Two - Transonic Flow

Author(s): Bernard Mazelsky; Harry B. Amey, Jr.
Corporate Author: Aeroject-General Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-11
Report Number: ASD TDR 62-155 Part 2
full text unavailable

Study to Determin Skin-Friction Drag in Hypersonic Low-Density Flow: Vlume I: Summary Analysis

Author(s): W. Leon Francis; Frank S. Malvestuto; Jay W. Stuart
Corporate Author: Lockheed-California Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-433 Volume 1
full text unavailable

A Theoretical And Experimental Investigation Of The Acoustic Response Of Cavities In An Aerodynamic Flow

Author(s): H. E. Plumblee, J. S. Gibson, L. W. Lassiter
Corporate Author: Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: WADD TR 61-75
full text available

New Approaches to Flight Vehicle Structural Vibration Analysis and Control

Author(s): Manfred A. Heckl; Richard H. Lyon; Gideon Maidanik; Eric E. Ungar
Corporate Author: Bolt, Beranek & Newman, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-237
full text unavailable

An Engineering Evaluation of Methods for the Prediction of Fatigue Life in Airframe Structures

Author(s): W. J. Crichlow; A. J. McCulloch
Corporate Author: Lockheed Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: ASD TR 61-434
full text unavailable

Advanced Concepts of Stochastic Processes and Statistics for Flight Vehicle Vibration Estimation and Measurement

Author(s): Julius S. Bendat; Loren D. Enochson; G. Harold Klein; Allan G. Piersol
Corporate Author: Thompson Ramo Wooldrige, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-973
full text unavailable

Optimum Fatigue Spectra

Author(s): G. S. Neuls
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: WADD TR 60-398
full text unavailable

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

Optimum Fatigue Spectra

Author(s): G. S. Neuls, H. G. Maier, T. R. Lerwick, E. A. Robb and I. J. Webster
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-235
full text unavailable

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