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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33 reports

Structural Design for Acoustic Fatigue


Corporate Author: Douglas Aircraft Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-10
Report Number: ASD TDR 63-820
full text available

Static Aerodynamic Characteristics at Mach 5 and 8 of an Aerodynamically Controllable Winged Re-Entry Configuration. Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Meckler, Lawrence
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: FDL TDR 64-10
full text available

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume I, Aerodynamics

Author(s): Batt, James R.
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: FDL TDR 64-16 Part 1 Volume 1
full text available

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics

Author(s): Batt, James R.
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: FDL TDR 64-16 Part 1 Volume 2
full text available

Design Criteria For Ground-Induced Dynamic Loads

Author(s): Hahn, Edward E.
Corporate Author: IIT Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: RTD TDR 63-4139 Volume 1
full text available

Design Criteria For Ground-Induced Dynamic Loads

Author(s): Hahn, Edward E.
Corporate Author: IIT Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: RTD TDR 63-4139 Volume 2
full text available

The Effect Of Plastic Deformation On The Strain Energy Release Rate In A Centrally Notched Plate Subjected To Uniaxial Tension

Author(s): Forman, Royce G.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1966-01
Report Number: AFFDL TR 65-186
full text available

High Altitude Critical Atmospheric Turbulence Data System

Author(s): Boone, Joseph P.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1967-05
Report Number: AFFDL TR 67-1
full text available

Investigation Of The High Pressure Electrodeless Arc In Air

Author(s): Hollister, Donald D.
Corporate Author: Philco-Ford Corp Newport Beach Calif Aeronutronic Div
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1969-02
Report Number: AFFDL TR 68-160
full text available

Flight Evaluation of Various Short Period Dynamics at Four Drag Configurations for the Landing Approach Task

Author(s): Chalk, Charles R.
Corporate Author: Cornell Aeronautical Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-60
full text available

Pressure Measurements at Mach 8 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Meckler, Lawrence
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report Number: FDL TDR 64-124
full text available

Heat Transfer Measurements at Mach 9 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Meckler, Lawrence
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: FDL TDR 64-142
full text available

Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle

Author(s): None Given
Corporate Author: Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Report Number: FDL TDR 64-32 Final Report
full text available

Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle

Author(s): None Given
Corporate Author: Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Report Number: FDL TDR 64-32 Summary Final Report
full text available

Lithium Spray Structural Cooling

Author(s): Mistretta, Andrew L.
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-11
Report Number: AFFDL TR 64-169
full text available

The Effects of Active Cooling on the Aerodynamic and Aerothermodynamic Characteristics of Slender Bodies of Revolution

Author(s): Leadon, B. M.
Corporate Author: General Dynamics/Convair
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report Number: AFFDL TR 64-187
full text available

Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Volume II. - Structral Loads Formulation

Author(s): Mann, C. D.
Corporate Author: McDonnell Aircraft Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report Number: FDL TDR 64-1 Part 1 Volume 2
full text available

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity

Author(s): Batt, James R.
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-16 Part 2
full text available

The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations

Author(s): Brook, John W.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report Number: FDL TDR 64-7
full text available

Development of the Shim Joint Concept for Composite Structural Members

Author(s): Cole, B. W.
Corporate Author: Bedix Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1967-08
Report Number: AFFDL TR 67-116
full text available

Analytical and Experimental Investigation of the Acoustic Environment of the RTD Sonic Fatigue Main Test Chamber

Author(s): Tyzzer, Franklin G.
Corporate Author: IIT Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: FDL TDR 64-26
full text available

Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles - II

Author(s): Kishi, F. H.
Corporate Author: University of California
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report Number: FDL TDR 64-48 Part 1
full text available

Development and Flight Calibration of a Variable-Drag Device on a Variable Stability T-33 Airplane

Author(s): Newell, F. D.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 62-910
full text available

Model Fly Program, Part I. Theoretical Investigations and Preliminary Design Considerations

Author(s): Hill, J. A.
Corporate Author: Giannini Controls Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report Number: FDL TDR 64-49 Part 1
full text available

Carbon Monoxide Management, Part I: Technique for Carbon Dioxide Absorber Evaluation

Author(s): Allen, John P.
Corporate Author: AF Air Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-06
Report Number: FDL TDR 64-67 Part 1
full text available

Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique

Author(s): Padlog, Joseph
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: FDL TDR 64-42
full text available

Structural Dynamic Response of Large Logistic V/STOL Vehicles

Author(s): Rich, M. J.
Corporate Author: Sikorsky Aircraft
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: FDL TDR 64-44
full text available

Low Frequency Instabilities of Free Systems

Author(s): Schwendler, Robert G.
Corporate Author: Computer Engineering Associates
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 63-655
full text available

Research on Accelerated Reliability Testing Methods Applicable to Non-Electronic Components of Flight Control Systems

Author(s): Johnson, W. F.
Corporate Author: Curtiss-Wright Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-03
Report Number: AFFDL TR 64-181
full text available

Investigation of Catalytic Reactions for CO2 Reduction, Part I - Evaluation of a Nickel-Kieselguhr Catalyst

Author(s): Thompson, Edward B., Jr.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-22 Part 1
full text available

Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls

Author(s): Kaufman, Louis G., II
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report Number: FDL TDR 64-120
full text available

Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate

Author(s): Kaufman, Louis G., II
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: RTD TDR 63-4044 Part 3
full text available

Two Dimensional Analysis of Transient Heat Conduction in a Sector of a Hollow Circular Cylinder

Author(s): Torian, J. G.
Corporate Author: Martin Company Aerosciences Research Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 63-642
full text available