24 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
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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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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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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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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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
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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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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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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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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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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A Rational Method for Predicting Alighting Gear Dynamic Loads: Volume II: Examples
Author(s): Ferguson, T. R. Corporate Author: Chance Vought Corporation Laboratory: AF Flight Dynamics Laboratory Date of Publication: 1963-12 Report Number: ASD TDR 62-555 Volume II
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A Rational Method for Predicting Alighting Gear Dynamic Loads: Volume I: General Methods
Author(s): Ferguson, T. R. Corporate Author: Chance Vought Corporation Laboratory: AF Flight Dynamics Laboratory Date of Publication: 1963-12 Report Number: ASD TDR 62-555 Volume I
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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
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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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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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