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64 reports
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
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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Investigation of a Close Tolerance Pyrotechnic Metallic Delay Element
Author(s): Peterson, W. R. Corporate Author: Frankford Arsenal Laboratory: AF Flight Dynamics Laboratory Date of Publication: 1963-09 Report Number: ASD TDR 63-563
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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
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
Automatic Runway Profile Measuring Instrumentation And Runaway Properties. Part III: Base Surveys
Author(s): Turner, D. F. Corporate Author: Midwest Research Institute Laboratory: AF Flight Dynamics Laboratory Date of Publication: 1963-07 Report Number: WADD TR 60-470 Part III AD Number: AD0415618
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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
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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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
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
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
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
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
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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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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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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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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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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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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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
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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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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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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
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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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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
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
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
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
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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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
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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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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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
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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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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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
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
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
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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
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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
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
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
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
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
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