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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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 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
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