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- 1965 (170)
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170 reports
A Study of the Influence of Lubricants on High-Speed Rolling-Contact Bearing Performance: Part V. Research on Elastohydrodynamic Lubrication on High-Speed Rolling Contacts
Author(s): Kannel, Jerrold Corporate Author: Battelle Memorial Institute Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-07 Report Number: ASD TDR 61-643 Part 5
Research on Gas Lubrication at High Temperatures and Low Flow Rates
Author(s): Lewis, P. Corporate Author: Mechanical Technology, Inc. Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-03 Report Number: APL TDR 64-56 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
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
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
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
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
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
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
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
Development of Space Expanded and Rigidized Solar Energy Collectors
Author(s): Schwartz, S. Corporate Author: Hughes Aircraft Company Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 555-571
Aluminum Foil Expandable Structures
Author(s): Motta, S. Corporate Author: Avco Corporation Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 572-602
Fabrication and Pressurization Technology for Improvement of Surface Accuracy of Passive Communications Satellites
Author(s): Grana, D. C. Corporate Author: NASA Langley Research Center Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 603-616
Astronaut Maneuvering Unit Technology
Author(s): Van Schaik, P. N. Corporate Author: Air Force Aero Propulsion Laboratory Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 633-648
Deployment System for the Pegasus Meteoroid Technology Satellite
Author(s): Ganssle, E. R. Corporate Author: Fairchild Hiller Corp. Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 649-657
Structural Behavior of Tapered Inflated Fabric Cylinders Under Various Loading Conditions
Author(s): Kovalesvsky, L. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 659-685
Satellite Applications for Expandable Space Structures
Author(s): Zahn, H. S. Corporate Author: Martin Company Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 687-707
Recent Applications of Inflated Structures to Aerospace Vehicles
Author(s): Ross, R. S. Corporate Author: Good Year Space Corp. Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 709-739
Correlation of Analytical and Experimental Results of Cylindrical Shells Under Newtonian Pressure Distribution
Author(s): Lycurgus, N. C. Corporate Author: None Given Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 740-767
High-Temperature Protective Re-entry Coatings for Expandable Structures
Author(s): Conger, M. T. Corporate Author: None Given Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 769-783
Dual Wall Inflatable Structures for Space Oriented Applications
Author(s): Bair, H. Q. Corporate Author: Air Inflatable Products Corporation Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 785-802
Introduction and Table of Contents
Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. i-xiii
Membrane Analysis of Pressurized Thin Spheroid Shells Composed of Flat Gores and Its Application to Echo II
Author(s): Bahiman, H. Corporate Author: None Given Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1965-05-27 Report Number: AFAPL TR 65-108 p. 617-631
The Evolution of USAF Environmental Testing
Author(s): Junker, V. J. Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1965-10 Report Number: AFFDL TR 65-197
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
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
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
Application of Lyapunov's Direct Method to Stability Problems in Elastic and Aeroelastic Systems
Author(s): Wang, P. K. C. 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): Wang, P. K. C. 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
Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method
Author(s): Wang, P. K. C. 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. 72-83
Optimum Control of a Class of Mixed Distributed and Lumped Parameter Systems
Author(s): Wang, P. K. C. 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. 84-106
Estimates for Truncation Errors of Infinite Dimensional Systems of Linear Ordinary Differential Equations
Author(s): Brady, M. L. 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. 107-126