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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30 reports

A Study Of The Characteristics O Fmodern Engine Noise And The Response Characteristics Of Structures

Author(s): R. J. Cox, H. J. Parry, J. Clough
Corporate Author: Lockheed Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: WADD TR 60-220
full text unavailable

Investigation Of Thermal Effects On Structural Fatigue


Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report Number: WADD TR 60-410 Part 2
full text unavailable

Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program

Author(s): Robert C. Brown; Robert V. Brulle; Gerald D. Giffin
Corporate Author: McDonnell Aircraft Corporation, St. Louis, Missouri
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-05
Report Number: WADD TR 60-781 Part 1
full text unavailable

Multiwall Structures For Space Vehicles

Author(s): S. Lampert; D. G. Younger
Corporate Author: Aeronutronic, A Division of Ford Motor Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-05
Report Number: WADD TR 60-503
full text unavailable

Investigation Of Thermal Effects On Structural Fatigue


Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-08
Report Number: WADD TR 60-410 Part 1
full text unavailable

Time-Dependant, Elasto-Plastic Bending Analysis For Structures Under Arbitrary Load-Temperature Environments. Part I: Analysis Development And Digital Program

Author(s): P. C. Huang
Corporate Author: The Martin Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-04
Report Number: WADD TR 60-541 Part 1
full text unavailable

Time-Dependant, Elasto-Plastic Bending Analysis For Structures Under Arbitrary Load-Temperature Environments. Part II: Experimental Verification

Author(s): C. J. Van Der Mass
Corporate Author: The Martin Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-04
Report Number: WADD TR 60-541 Part 2
full text unavailable

Similarity Studies For Dissociating Gases In Hypersonic , Low Density Flow

Author(s): K.Pearce, S.Samet And R.J.Whalen
Corporate Author: Flight Sciences Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-09
Report Number: WADD TR 60-341
full text unavailable

Response of Missile Structures to Impulse Loading

Author(s): T. Wah; L. U. Rastrelli; N. L. Basdekas; R. C. DeHart
Corporate Author: Southwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report Number: ASD TDR 62-475
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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
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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
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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
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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

Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program: Part 2 User's Manual

Author(s): Frederick W. Seubert; Newell E. Usher
Corporate Author: McDonnel Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-05
Report Number: WADD TR 60-781 Part 2
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
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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
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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

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 1. Summary of Technical Work

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 1
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 2. Measurement Techniques for Experimental Modal Analysis

Author(s): Randall J. Allenmang; David L. Brown; Robert W. Rost
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 2
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 3. Modal Parameter Estimation

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 3
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 4. System Modeling Techniques

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 4
full text unavailable

Experimental Modal Analysis and Dynamic Component Synthesis. Volume 5. Universal File Formats

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 5
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
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 6. Software User's Guide

Author(s): Randall J. Allenmang; David L. Brown
Corporate Author: University of Cincinnati
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-12
Report Number: AFWAL TR 87-3069 Volume 6
full text unavailable

A Handling Qualities Study of Integrated Flight/Fire Control (IFFC)

Author(s): Cord, Thomas J.
Corporate Author: Control Dynamics Branch, Flight Control Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1981-03
Report Number: AFWAL-TM-81-68-FIGC
full text unavailable

Design Guide for Bolted Joints in Composite Structures

Author(s): R. L. Ramkumar; E. S. Saether; D. Cheng
Corporate Author: Northrup Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1986-03-01
Report Number: AFWAL TR 86-3035
full text unavailable