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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
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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
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
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
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
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
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
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
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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
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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
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
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
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
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
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
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
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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
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
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
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
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
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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
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
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
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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
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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
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
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
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
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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
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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
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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
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
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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
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
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
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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
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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
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
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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
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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
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
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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
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
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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
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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
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
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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
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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
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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
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