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

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

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

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

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

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

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

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

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

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

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

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

Altimeter Display Study Part I. Summary and Review of Data Requirements

Author(s): Matheny, W. G.
Corporate Author: Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: ASD TDR 63-621 Part 1
full text by request

Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures

Author(s): Roberts, W. H.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report Number: ASD TDR 62-801 Supplement I
full text by request

Extension of Linear Constant-Coefficient Analysis Methods to Time-Varying Systems

Author(s): Johnson, Walter A.
Corporate Author: Systems Technology, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: RTD TDR 63-4178
full text by request

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

Flat-Plate Boundary-Layer Transition at Hypersonic Speeds

Author(s): Deem, R. E.
Corporate Author: Douglas Aircraft Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-129
full text unavailable