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

Investigation of a Close Tolerance Pyrotechnic Metallic Delay Element

Author(s): W. R. Peterson
Corporate Author: Frankford Arsenal
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-563

Low Frequency Instabilities of Free Systems

Author(s): Robert G. Schwendler and Jack H. Hill
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

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

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

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): Louis G. Kaufman
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-755

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): L. L. Mazzola; J. Putukian; E. S. Criscione; N. P. Hobbs
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 62-908

Research and Study of Analytical Techniques for Predicting Reliability of Flight-Control Systems

Author(s): L.H. Stember; D. G. Mark; R. E. Mesloh; A. A. Putnam
Corporate Author: Battelle Memorial Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 63-287

Investigation of Techniques for Predicting the Development Cost and Development Time of Automatic Flight Control Systems

Author(s): R. A. Courtney; H. M. Dye; R. L. Erler; C. P. Martin; F. C. Reed; H. T. Spiro; D. E. Johnston
Corporate Author: Planning Research Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 62-751

Demonstration of the Application of Majority Logic for Increased Reliability in Automatic Flight Control Systems

Author(s): R. M. Derby; J. J. Fleck
Corporate Author: General Electric Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-275

A Rational Method for Predicting Alighting Gear Dynamic Loads: Volume II: Examples

Author(s): T. R. Ferguson, J. Mollick and W. W. Kitts
Corporate Author: Chance Vought Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-12
Report Number: ASD TDR 62-555 Volume II

A Rational Method for Predicting Alighting Gear Dynamic Loads: Volume I: General Methods

Author(s): T. R. Ferguson, J. Mollick and W. W. Kitts
Corporate Author: Chance Vought Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-12
Report Number: ASD TDR 62-555 Volume I

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

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

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

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

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

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

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