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35 reports
Format-Fortran Matrix Abstraction Technique. Volume V - Supplement I. Engineering User and Technical Report - Extended.
Author(s): Pickard, J. Corporate Author: Douglas Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume V Supplement I
Format-Fortran Matrix Abstraction Technique. Volume VI. Supplement I. Description of Digital Computer Program. Phase I. Extended.
Author(s): Morris, R.C. Corporate Author: Douglas Aircraft Company, Long Beach, California Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume VI Supplement I
Format-Fortran Matrix Abstraction Technique. Volume VII - Supplement I. Description of Digital Computer Program - Phase III - Extended.
Author(s): Frank, J. A. Corporate Author: Douglas Aircraft Company, Long Beach, California Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume VII Supplement I
Research on Elastohydrodynamic Lubrication on High-Speed Rolling-Sliding Contacts
Author(s): Smith, Richard L. Corporate Author: Mechanical Technology, Inc. Latham, New York Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1970-12 Report Number: AFAPL TR 71-54
A Wind Tunnel Investigation of Jets Exhausting into a Crossflow: Volume IV: Additional Data for the Three-Jet Configuration
Author(s): Fricke, L. B. Corporate Author: Northrop Corporation, Aircraft Division Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-12 Report Number: AFFDL TR 70-154 Volume 4
A Discrete, Stochastic, Optimal Control Model of the Human Operator in a Closed-Loop Tracking Task
Author(s): Paskin, Harvey M. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-11 Report Number: AFFDL TR 70-129
A Wind Tunnel Investigation of Jets Exhausting into a Crossflow
Author(s): Fricke, L. B. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-12 Report Number: AFFDL TR 70-154 Volume 3
An In-Flight Invesitgation to Develop Control System Design Criteria for Fighter Airplanes
Author(s): Neal, T. Peter Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-12 Report Number: AFFDL TR 70-74 Volume 1
A Wind Tunnel Investigation of Jets Exhausting into a Crossflow
Author(s): Fricke, L. B. Corporate Author: Northrop Corporation, Aircraft Division Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-12 Report Number: AFFDL TR 70-154 Volume 1
A Wind Tunnel Investigation of Jets Exhausting into a Crossflow
Author(s): Fricke, L. B. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-12 Report Number: AFFDL TR 70-154 Volume 2
Studies on the Behavior of Nickel-Base Superalloys at High Temperatures
Author(s): Kvernes, Ingard Corporate Author: Central Institute for Industrial Research Laboratory: Materials Laboratory Date of Publication: 1970-07 Report Number: AFML TR 70-103
Analysis of Data Density and Storage Requirements for High Resolution Radar Simulation System Design
Author(s): Fligor, Patrick D. Corporate Author: Technology Incoporated Laboratory: Air Force Human Resources Laboratory Date of Publication: 1970-06 Report Number: AFHRL-TR-70-12
Corrosion Cracking of Metallic Materials
Author(s): Fontana, Mars G. Corporate Author: Ohio State Univ Columbus Dept Of Metallurgical Engineering Laboratory: Air Force Materials Laboratory Date of Publication: 1970-01 Report Number: AFML TR 70-2
System Description and Performance Data for the USAF/CAL Variable Stability T-33 Airplane
Author(s): Hall, G. Warren Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 70-71
In-Flight Investigation of Lateral-Directional Dynamics for the Landing Approach
Author(s): Hall, G. Warren Corporate Author: Cornell Aeronautical Laboratory Inc., Buffalo, New York Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-10 Report Number: AFFDL TR 70-145
Design, Fabrication, and Flight Testing of Self-Organizing Flight Control System
Author(s): Barron, Roger L. Corporate Author: Adaptronics, Inc. McLean, Virginia Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-06 Report Number: AFFDL TR 70-77
Hypersonic Surface Pressure and Heat Transfer on Slender Bodies in Variable Composition and Nonequilibrium Atmospheres
Author(s): Harney, D. J. Corporate Author: Ohio Stat University Aeronautical and Astronautical Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-04 Report Number: AFFDL TR 70-31
Three-Dimensional Nozzle Design for Maximum Thrust. Volume I. Theoretical Development and Results
Author(s): Snyder, Lynn E, Corporate Author: Purdue University Jet Propulsion Center Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1970-10-28 Report Number: AFAPL TR 70-79 Volume 1
Basic Kinematics and Dynamics of the Humane Centrifuge and Other Aerospace Simulators, Including a Simple Explanation of Coriolis and Gyroscopic Effects
Author(s): Schueller, Otto Corporate Author: Aerospace Medical Research Laboratory Laboratory: Aerospace Medical Research Laboratory Date of Publication: 1970-05 Report Number: AMRL TR 69-126
A Stability and Control Prediction Method for Helicopters and Stoppable Rotor Aircraft. Volume I. Engineer's Manual
Author(s): Livingston, Charles L. Corporate Author: Bell Helicopter Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-02 Report Number: AFFDL TR 69-123 Volume 1
A Flight Investigation of Lateral-Directional Handling Qualities for V/STOL Aircraft in Low Speed Maneuvering Flight
Author(s): Doetsch, K-H. Corporate Author: National Aeronautical Establishment, Canada Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-03 Report Number: AFFDL TR 69-41
Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part IX - Calculation of Thermodynamic Quantities from Phase Diagrams
Author(s): Rudy, E. Corporate Author: Aerojet-General Corporation Laboratory: Air Force Materials Laboratory Date of Publication: 1970-08 Report Number: AFML TR 69-117 Part 9
Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part VII - The Phase Diagram Ti-V-C
Author(s): Rudy, E. Corporate Author: Aerojet-General Corporation Laboratory: Air Force Materials Laboratory Date of Publication: 1970-08 Report Number: AFML TR 69-117 Part 7
Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part V - The Phase Diagram W-B-C
Author(s): Rudy, E. Corporate Author: Aerojet-General Corporation Laboratory: Air Force Materials Laboratory Date of Publication: 1970-08 Report Number: AFML TR 69-117 Part 5
Phase Equilibria Investigation of Binary, Ternary, and Higher Order Systems, Part I - The Phase Diagrams of the Systems Ti-Nb-C, Ti-Ta-C, and Ti-Mo-C
Author(s): Rudy, E. Corporate Author: Aerojet-General Corporation Laboratory: Air Force Materials Laboratory Date of Publication: 1970-08 Report Number: AFML TR 69-117 Part 1
Parametric Fatigue Analysis of USAF Fighter Aircraft
Author(s): Roth, George J. Corporate Author: University of Dayton Research Institute Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-01 Report Number: AFFDL TR 69-85
Stability Characterization of Refractory Materials Under High Velocity Atmospheric Flight Conditions. Part 3, Volume 3: Experimental Results of High Velocity Hot Gas/Cold Wall Tests.
Author(s): Kaufman, Larry Corporate Author: ManLabs Inc. Laboratory: Air Force Materials Laboratory Date of Publication: 1970-02 Report Number: AFML TR 69-84 Part 3 Volume 3
Prediction Of Supersonic Laminar Flow Separation By The Method Of Integral Relations With Free Interaction.
Author(s): Kuhn, Gary D. Corporate Author: Nielsen Engineering And Research Inc Palo Alto Calif Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-01 Report Number: AFFDL TR 69-87
Approximate Solution Of Plane Orthotropic Elasticity Problems5
Author(s): Schimke, Joel Corporate Author: Bell Aerosystems Co Buffalo N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-01 Report Number: AFFDL TR 69-84
Flight Test Evaluation of a Scratch Strain Gage.
Author(s): Haglage, Theodore L. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-06 Report Number: AFFDL TR 69-116
Crack Propogation in Aluminum Alloy Sheet Materials Under Flight-Simulation Loading
Author(s): Schijve, J. Corporate Author: National Aerospace Laborator, Amsterdam, The Netherlands Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-09 Report Number: AFFDL TR 69-50
Development of a Solid-State Display System
Author(s): Fisher, Archie L. Corporate Author: ITT Federal Laboratories Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-03 Report Number: AFFDL TR 68-133
Analysis of VTOL Handling Qualities Requirements: Part II. Lateral-Directional Hover and Transition
Author(s): Craig, Samuel J. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-02 Report Number: AFFDL TR 67-179 Part 2
Stability of Elastic Equilibrium
Author(s): Koiter, Warner Tjardus Corporate Author: Stanford University Department of Aeronautics and Astronautics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-02 Report Number: AFFDL TR 70-25
Study and Design of an Ejection System for VTOL Aircraft: Part I, Volume 3 - Computer Program User's Manual for VTOL Escape System Simulation
Author(s): Clinkenbeard, I. L. Corporate Author: Vought Aeronautics Division, LTV Aerospace Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-03 Report Number: AFFDL TR 70-1 Part 1 Volume 3