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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64 reports

Analytical and Experimental Investigation of Coated Metal Fabric Expandable Structures for Aerospace Applications

Author(s): None Given
Corporate Author: Goodyear Aerospace Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 63-542
full text by request

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

Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part II: Mach 5 Pressure Data for Flows Ahead of Ramps: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-679 Part 2
full text by request

Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-679 Part 1
full text unavailable

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

Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration

Author(s): Kaufman, Louis G., II
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-02
Report Number: RTD TDR 63-4179 Part 1
full text by request

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

Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity

Author(s): Gilmore, Arthur
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 62-460
full text unavailable

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

Altimeter Display Study Part II. Handbook for Static Testing of Altimeters

Author(s): Elam, C. B.
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-622 Part 2
full text by request

Altimeter Display Study Part III. Summary of Experimental Testing

Author(s): Elam, C. B.
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-623 Part 3
full text by request

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

The Effect of Surface Perturbations on the Pressure Distributions About Blunt Two-Dimensional Bodies at High Mach Numbers

Author(s): Donaldson, Coleman duP.
Corporate Author: Aeronautical Research Associates of Princeton, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: FDL TDR 64-17
full text by request

Study of a Servo Actuator Design and Test and Fabrication of an Experimental Model

Author(s): Banfield, R. T.
Corporate Author: Hydraulic Research and Manufacturing Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 62-620
full text by request

Digital Adaptive Flight Control System Phase II

Author(s): Andeen, R. E.
Corporate Author: Sperry Phoenix Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-854
full text by request

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

A Measurement of the Static Aeroelastic Deformation and Loading of a Wing in Supersonic Flow

Author(s): Durgin, F. H.
Corporate Author: Massachusetts Institute of Technology
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-366
full text by request

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

Simplified Analytical Methods for Use in Preliminary Design of Vertically-Rising Vehicles Subjected to Wind Shear Loads: Part II - Wind Statistics and Discrete Profiles

Author(s): Hobbs, N. P.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: FDL TDR 64-8 Part 2
full text unavailable

Simplified Analytical Methods for Use in Preliminary Design of Vertically-Rising Vehicles Subjected to Wind Shear Loads: Part I - Evaluation of Methods

Author(s): Hobbs, N. P.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: FDL TDR 64-8 Part 1
full text unavailable

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

Development of a Low Altitude Turbulence Model for Estimating Gust Loads on Aircraft

Author(s): Lappe, U. O.
Corporate Author: New York University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-318
full text unavailable

The Statistical Properties of Signals and Measurements of Simple Manual Control Systems

Author(s): Elkind, Jerome I.
Corporate Author: Bolt Beranek and Newman, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-85
full text by request

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

Research and Study of Analytical Techniques for Predicting Reliability of Flight-Control Systems

Author(s): Stember, L. H.
Corporate Author: Battelle Memorial Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 63-287
full text by request

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

Wind, wind Shear, and Gust design Criteria for Vertically-Rising Vehicles as Recommended on the Basis of Wind Data from Eleven United States and Foreign Locations

Author(s): Mazzola, L. L.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 62-908
full text unavailable

Pressure Distributions and Oil Film Photographs for Mach 5 Flows Past Fins Mounted on a Flat Plate: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-755
full text by request

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

Preliminary Design Considerations for a V/STOL Wind Tunnel

Author(s): Knowlton, Marcus P.
Corporate Author: Princeton University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-01
Report Number: FDL TDR 64-146
full text by request

Three-Degree-of-Freedom Problem Optimization Formulation Volume 3 - User's Manual

Author(s): Mobley, R. L.
Corporate Author: McDonnell Aircraft Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-06
Report Number: FDL TDR 64-1 Part 2 Volume 3
full text by request

Demonstration of the Application of Majority Logic for Increased Reliability in Automatic Flight Control Systems

Author(s): Derby, R. M.
Corporate Author: General Electric Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-275
full text by request

Investigation of Techniques for Predicting the Development Cost and Development Time of Automatic Flight Control Systems

Author(s): Courtney, R. A.
Corporate Author: Planning Research Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 62-751
full text unavailable

Empirical Correlation of Excitation Environment and Structural Parameters with Flight Vehicle Vibration Response

Author(s): White, R. W.
Corporate Author: Northrup Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report Number: AFFDL TR 64-160
full text by request