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533 reports
Analysis of the Probability of Collapse of a Fail-Safe Aircraft Structure Consisting of Parallel Elements
Author(s): S. Eggwertz; G. Lindsjo 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): Louis G. Kaufman 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): James R. Batt 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): C. L. Tai, L. V. Andrew, M. M. H. Loh, P. C. Kamrath 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): Kempton A. Toups Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-04 Report Number: FDL TDR 64-43
Fixed-Base and In-Flight Simulations of Longitudal and Lateral-Directional Handling Qualities for Piloted Re-Entry Vehicles
Author(s): Edwin A. Kidd, Robert P. Harper, Jr. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1964-02 Report Number: ASD TDR 61-362
An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman II; Lawrence Meckler; Stavros A. Hartofilis; Daniel Weiss 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): T. C. Li 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): M. T. Moore; L. V. Andrew 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): E. R. Rodemich; L. V. Andrew 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): H. T. Vivian; L. V. Andrews 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): Louis G. Kaufman 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): Louis G. Kaufman 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): Louis G. Kaufman 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): J. D. Ingram 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): J. C. Samuels 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): William J. Evans; Louis G. Kaufman II 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): J. A. Thelander 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): Gibbs S. Raetz; W. Byron Brown 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): Robert L. Swaim 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): R. L. Barnoski 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): S. J. Lis, R. G. Barile and G. Engholm 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): A. P. Coppa and W. A. Nash 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): J. S. Keith and J. W. Lincoln 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): Glendon R. Crump, Lt, USAF 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): G. P. Thrall 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): Helmut G. Heinrich and Lelan R. Jamison, Jr. 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): R. B. Hobbs, 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): H. Rie, E. A. Linkiewicz and F. D. Bosworth 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): L. V. Andrew and T. E. Stenton 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): C. J. Cohan, G. Campbell, W. Herman, W. Nugent and J. Heathman 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): Ronald D. Kelly 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): Robert J. Woodcock; Douglas E. Drake 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): Duan McRuer; Dunstan Graham; Ezra Krendel; William Reisener, Jr. 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): James A. Payne 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): N. R. Goodman Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-06 Report Number: AFFDL TR 65-56
Tests for Randomness, Stationarity, Normality and Comparison of Spectra
Author(s): J. S. Bendat; L. D. Enochson; A. G. Piersol 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): R. L. Stapleford; J. Wolkovitch; R. E. Magdaleno; C. P. Shortwell; W. A. Johnson 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): R. D. Kelly 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): R. D. Kelly 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): Jack N. Nielsen; Larry L. Lynes; Frederick K. Goodwin 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): Jack N. Nielsen; Larry L. Lynes; Frederick K. Goodwin 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): I. L. Ashkenas 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): I. L. Ashkenas 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): G. Kurylowich 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): Leon H. Schindel 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
Application of Lyapunov's Direct Method to Stability Problems in Elastic and Aeroelastic Systems
Author(s): P. K. C. Wang 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. 29-64
Asymptotic Stability of Equilibrium of a Simplified Aerodynamic Vehicle with Flexible Tail
Author(s): P. K. C. Wang 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. 65-71