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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12 reports

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

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

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

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

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