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): 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

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

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

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