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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27 reports

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

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

Study of a Sonic Load Recorder, Volume I.

Author(s): Ball, Jay H.
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

Structural Flight Loads Data from F-106A Aircraft

Author(s): Vahldiek, Artie
Corporate Author: Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TDR 62-246
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): Mazelsky, Bernard
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

Further Studies on High-Speed Unsteady Flow

Author(s): Zartanian, Garabed
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

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

Author(s): Bendat, Julius S.
Corporate Author: Thompson Ramo Wooldrige, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-12
Report Number: ASD TDR 62-973
full text unavailable

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

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

Optimum Fatigue Spectra

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

Strength, Efficiency, and Design Data for Beryllium Structures

Author(s): Crawford, Robert F.
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

On Developing a Low Altitude Turbulence Model for Aircraft Gust Loads

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

Optimum Fatigue Spectra

Author(s): Neuls, G. S.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report Number: ASD TR 61-235
full text unavailable

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

Author(s): Fitch, G. E.
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

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

Author(s): Fuller, J. R.
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

Practical Aspects of Aerothermoelastic Modelling

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

New Approaches to Flight Vehicle Structural Vibration Analysis and Control

Author(s): Heck, Manfred A.
Corporate Author: Bolt, Beranek & Newman, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-237
full text unavailable

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

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

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

Author(s): Eggwertz, Sigge
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

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

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

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

Author(s): Francis, W. Leon
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

Survey and Evaluation of Sonic Fatigue Testing Facilities

Author(s): Bianchi, Ralph A.
Corporate Author: CONESCO Consultants in Engineering Science
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: ASD TR 61-185
AD Number: AD0277124
full text by request

Thermo-Structural Analysis Manual

Author(s): Forray, M. J.
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

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

Author(s): Ruetenik, J. Ray
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

Methods For Analyzing Flight Vehicles During The Taxi Condition

Author(s): Theisen, J. G.
Corporate Author: Lockheed-Georgia Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-01
Report Number: ASD TR 61-177
AD Number: AD0273305
full text by request

Prediction Of Creep Effects In Aircraft Structures

Author(s): Alesch, C. W.
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

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

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

Thermo-Structural Analysis Manual

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