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560 reports
Fixed-Base and In-Flight Simulations of Longitudal and Lateral-Directional Handling Qualities for Piloted Re-Entry Vehicles
Author(s): Kidd, Edwin A. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-02 Report Number: ASD TDR 61-362
Analysis of the Probability of Collapse of a Fail-Safe Aircraft Structure Consisting of Parallel Elements
Author(s): Eggwertz, S. Corporate Author: Aeronautical Research Institute of Sweden Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-02 Report Number: RTD TDR 63-4210
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part II" Pressure Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-09 Report Number: FDL TDR 64-2 Part 2
Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Author(s): Batt, James R. Corporate Author: Bell Aerosystems Co. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-02 Report Number: FDL TDR 64-16 Part 3
Transient Dynamic Response of Orbiting Space Stations
Author(s): Tai, C. L. Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-02 Report Number: FDL TDR 64-25
Confac II, A General Computer Program for the Determination of Radiant-Interchange Configuration and Form Factors
Author(s): Toups, Kempton A. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-04 Report Number: FDL TDR 64-43
Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Problem Formulation
Author(s): Brown, Robert C. Corporate Author: McDonnell Aircraft Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-10 Report Number: FDL TDR 64-1 Part 1 Volume 1
An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-01 Report Number: AFFDL TR 64-174
Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack
Author(s): Li, T. C. Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: FDL TDR 64-152 Part 5
Unsteady Aerodynamics for Advanced Configurations: Part IV - Application of the Supersonic Mach Box Method to Intersecting Planar Lifting Surfaces
Author(s): Moore, M. T. Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: FDL TDR 64-152 Part 4
Unsteady Aerodynamics for Advanced Configurations: Part II - A Transonic Box Method for Planar Lifting Surfaces
Author(s): Rodemich, E. R. Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: FDL TDR 64-152 Part 2
Unsteady Aerodynamics for Advanced Configurations: Part I - Application of the Subsonic Kernel Function to Nonplanar Lifting Surfaces
Author(s): Vivian, H. T. Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: FDL TDR 64-152 Part 1
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part I: Pressure Data for Delta Wing Surface
Author(s): Kaufman, Louis G., II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-01 Report Number: FDL TDR 64-2 Part 1
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface
Author(s): Kaufman, Louis G., II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-05 Report Number: FDL TDR 64-2 Part 3
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part IV: Heat Transfer Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-05 Report Number: FDL TDR 64-2 Part 4
A Survey of Aerodynamic Noise
Author(s): Ingram, J. D. Corporate Author: General Technology Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-12 Report Number: FDL TDR 64-132
Theoretical Studies of Methods of Generating Random Waves from Harmonic Sources
Author(s): Samuels, J. C. Corporate Author: General Technology Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-12 Report Number: FDL TDR 64-133
Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Evans, William J. Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-09 Report Number: FDL TDR 64-128
Aircraft Motion Analysis
Author(s): Thelander, J. A. Corporate Author: Douglas Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-03 Report Number: FDL TDR 64-70
Theoretical Investigations of Boundary Layer Stability
Author(s): Raetz, Gibbs S. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 64-184
Active Control of Booster Elasticity
Author(s): Swaim, Robert L. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-04 Report Number: AFFDL TR 64-189
Response of Elastic Structures to Deterministic and Random Excitation
Author(s): Barnoski, R. L. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: AFFDL TR 64-199
Window Systems for Advanced Vehicles
Author(s): Lis, S. J. Corporate Author: General American Transportation Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-12 Report Number: FDL TDR 64-39
Dynamic Buckling of Shell Structures Subject to Longitudinal Impact
Author(s): Coppa, A. P. Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-12 Report Number: FDL TDR 64-65
Methods in Structural Dynamics for Thin Shell Clustered Launch Vehicles
Author(s): Keith, J. S. Corporate Author: LTV Astronautics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-04 Report Number: FDL TDR 64-105
Aerodynamic Heating Simulation: Part I. Theory and Program Definition
Author(s): Crump, Glendon R. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-09 Report Number: FDL TDR 64-112 Part 1
An Analysis of Amplitude Probability Measurements
Author(s): Thrall, G. P. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-03 Report Number: FDL TDR 64-116
Stress Analysis of a Parachute During Inflation and at Steady State
Author(s): Heinrich, Helmut G. Corporate Author: University of Minnesota Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-02 Report Number: FDL TDR 64-125
Hypersonic Dynamic Stability: Part II. Conical Body Experimental Program
Author(s): Hobbs, R. B., Jr. Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-01 Report Number: FDL TDR 64-149 Part 2
Hypersonic Dynamic Stability: Part III. Unsteady Flow Field Program
Author(s): Rie, H. Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-01 Report Number: FDL TDR 64-149 Part 3
Unsteady Aerodynamics for Advanced Configurations: Part VII - Velocity Potentials in Non-Uniform Transonic Flow Over a Thin Wing
Author(s): Andrew, L. V. Corporate Author: North American Rockwell Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-08 Report Number: FDL TDR 64-152 Part 7
High Temperature Investigation of Various Crew Escape Concepts for the Reentry Flight Regime
Author(s): Cohan, C. J. Corporate Author: General Dynamics Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-11 Report Number: AFFDL TR 64-161
Transducers for Sonic Fatigue Measurements
Author(s): Kelly, Ronald D. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-02 Report Number: AFFDL TR 64-171
Estimation of Flying Qualities of Piloted Airplanes
Author(s): Woodcock, Robert J. Corporate Author: Douglas Aircraft Co. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 65-218
Human Pilot Dynamics in Compensatory Systems: Theory, Models, and Experiments with Controlled Element and Forcing Function Variations
Author(s): McRuer, Duane Corporate Author: Systems Technology, Inc.; The Franklin Institute Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-07 Report Number: AFFDL TR 65-15
Computational Methods in Optimal Control Problems
Author(s): Payne, James A. Corporate Author: University of California Department of Engineering Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-08 Report Number: AFFDL TR 65-50
Measurement of Matrix Frequency Response Functions and Multiple Coherence Functions
Author(s): Goodman, N. R. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-06 Report Number: AFFDL TR 65-56
Aerodynamics of a Rectangular Wing with a Peripheral Jet for Air Cushion Take-Off and Landing
Author(s): Dau, K. Corporate Author: University of Toronto Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-09 Report Number: AFFDL TR 65-59
Tests for Randomness, Stationarity, Normality and Comparison of Spectra
Author(s): Bendat, J. S. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-08 Report Number: AFFDL TR 65-74
An Analytical Study of V/STOL Handling Qualities in Hover and Transition
Author(s): Stapleford, R. L. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-10 Report Number: AFFDL TR 65-73
Evaluation Tests for Statistical Analyzers
Author(s): Kelly, R. D. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-06 Report Number: AFFDL TR 65-93
Systems for the Collection and Analysis of Dynamic Data
Author(s): Kelly, R. D. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-08 Report Number: AFFDL TR 65-94
Calculation of Laminar Separation with Free Interaction by the Method of Integral Relations: Part I - Two-Dimensional Supersonic Adiabatic Flow
Author(s): Nielsen, Jack N. Corporate Author: Itek Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-10 Report Number: AFFDL TR 65-107
Calculation of Laminar Separation with Free Interaction by the Method of Integral Relations: Part II - Two-Dimensional Supersonic Nonadiabatic Flow and Axisymmetric Supersonic Adiabatic and Nonadiabatic Flows
Author(s): Nielsen, Jack N. Corporate Author: Itek Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-107 Part 2
A Study of Conventional Airplane Handling Qualities Requirements: Part I. Roll Handling Qualities
Author(s): Ashkenas, I. L. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11 Report Number: AFFDL TR 65-138 Part 1
A Study of Conventional Airplane Handling Qualities Requirements: Part II. Lateral-Directional Oscillatory Handling Qualities
Author(s): Ashkenas, I. L. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11 Report Number: AFFDL TR 65-138 Part 2
The Light-Line-Tethering Technique for Determining the Aerodynamic Derivatives of an Air Cushion Vehicle
Author(s): Kurylowich, G. Corporate Author: University of Toronto Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 65-159
An Evaluation of Procedures for Calculating Aerodynamic Loads
Author(s): Schindel, Leon H. Corporate Author: Massachusetts institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: AFFDL TR 65-18
Table of Contents
Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. i-iv
Introduction
Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 1-4