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209 reports
Thermo-Structural Analysis Manual
Author(s): Forray, M. J. Corporate Author: Republic Aviation Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: WADD TR 60-517 Vol II
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. I. Surface Pressure Distributions on a Blunted Flat Plate
Author(s): Gregorek, G. M. Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-03 Report Number: ASD TDR 62-792 Volume 1
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. II. Laminar Boundary Layer Profile on the Flat Plate
Author(s): Gregorek, G. M. Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-03 Report Number: ASD TDR 62-792 Volume 2
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NB-66B High Altitude Gust Survey Technical Analysis, Volume I.
Author(s): Strom, J. A. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-04 Report Number: ASD TDR 63-145 Volume 1
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NB-66B High Altitude Gust Survey Power Spectra, Volume II.
Author(s): Strom, J. A. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-04 Report Number: ASD TDR 63-145 Volume 2
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NB-66B High Altitude Gust Survey Time Series, Volume III.
Author(s): Strom, J. A. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-04 Report Number: ASD TDR 63-145 Volume 3
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Prediction Of Creep Effects In Aircraft Structures
Author(s): Alesch, C. W. Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: WADD TR 60-411 Part 2
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Methods For Analyzing Flight Vehicles During The Taxi Condition
Author(s): Theisen, J. G. Corporate Author: Lockheed-Georgia Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-01 Report Number: ASD TR 61-177 AD Number: AD0273305
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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
Application Of The Subdomain (Biezeno-Koch) Method To Circular Plate Bending
Author(s): Adams, O. E., Jr Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1967-06 Report Number: AFFDL TR 66-215
Measurement Of The Diffraction Correction Of The Gulton Model P420m-6 Microphone
Author(s): Ortega, Jose C. Corporate Author: Western Electro-Acoustic Lab Inc Santa Monica CA Laboratory: Flight Dynamics Laboratory Date of Publication: 1967-05 Report Number: AFFDL TR 66-223
Investigation of High-Angle-of-Attack Maneuver-Limiting Factors Part II. Piloted Simulation Assessment of Bihrle Departure Criteria
Author(s): Mitchell, David G. Corporate Author: Systems Technology, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1980-12-01 Report Number: AFWAL TR 80-3141 Part 2
Investigation of High-Angle-of-Attack Maneuver-Limiting Factors Part III Appendices - Aerodynamic Models
Author(s): Mitchell, David G. Corporate Author: Systems Technology, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1980-12-01 Report Number: AFWAL TR 80-3141 Part 3
Characteristics of High Performance Ejectors
Author(s): Minardi, J. E. Corporate Author: University of Dayton Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 1982-01-01 Report Number: AFWAL TR 81-3170
Background Information and User Guide for MIL-F-8785C, Military Specification - Flying Qualities of Piloted Airplanes
Author(s): Moorhouse, David J. Corporate Author: Control Dynamics Branch, Flight Control Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1982-07-01 Report Number: AFWAL TR 81-3109
A Source-Doublet Approach to Modeling Triple Ejector Rack Store Configurations and Force Calculations
Author(s): Dyer, Calvin L. Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1981-07-01 Report Number: AFWAL TR 81-3059
Lateral Flying Qualities of Highly Augmented Fighter Aircraft
Author(s): Monagan, Stephen J. Corporate Author: Calspan Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1982-06 Report Number: AFWAL TR 81-3171 Volume 1
Lateral Flying Qualities of Highly Augmented Fighter Aircraft
Author(s): Monagan, Stephen J. Corporate Author: Calspan Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1982-06 Report Number: AFWAL TR 81-3171 Volume 2
A Graphic Method for Predicting Audibility of Noise Sources
Author(s): Fidell, Sanford Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1982-0-01 Report Number: AFWAL TR 82-3086
Suggested Revisions to MIL-F-8785C for Large (Class III) Aircraft
Author(s): Meyer, Robert T. Corporate Author: Lockheed-Georgia Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1983-02-01 Report Number: AFWAL TR 83-3015
Validation of USAF Stability and Control Datcom Methodologies for Straight-Tapered Sweptforward Wings
Author(s): Sharpes, Daniel G. Corporate Author: Design Prediction Group Laboratory: Flight Dynamics Laboratory Date of Publication: 1985-07-01 Report Number: AFWAL TR 84-3084
Post Stall Maneuvers and Thrust Vectoring Performance Analysis
Author(s): Miller, L. Earl Corporate Author: Highspeed Performance Branch, Aeromechanics Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1984-07-01 Report Number: AFWAL TR 84-3109
A Study of Aerodynamic Control in Stalled Flight Long Laminar Separation Bubble Analysis
Author(s): Dvorak, F. A. Corporate Author: Analytical Methods, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1985-02-01 Report Number: AFWAL TR 84-3091
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A Study of Aerodynamic Control in Stalled Flight Leading-Edge Vortex Formation Analysis
Author(s): Nathman, James K. Corporate Author: Analytical Methods, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1985-02-01 Report Number: AFWAL TR 84-3090
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V/STOL Concepts and Developed Aircraft. Volume 1. A Historical Report (1940-1986)
Author(s): Lindenbaum, B. Corporate Author: Universal Energy Systems Laboratory: Flight Dynamics Laboratory Date of Publication: 1986-11 Report Number: AFWAL TR 86-3071 Volume 1
An Investigation of Wing Lift Augmentation with Spanwise Tip Blowing
Author(s): Mendenhall, Michael R. Corporate Author: Nielsen Engineering & Research, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-04-22 Report Number: AFWAL TR 86-3112
Experimental Investigation of the Short-Period Requirements of MIL-F-8785C
Author(s): Bailey, Randall E. Corporate Author: ARVI/CALSPAN Advanced Technology Center Laboratory: Flight Dynamics Laboratory Date of Publication: 1986-11-01 Report Number: AFWAL TR 86-3109 Volume 1
Design Guide for Bolted Joints in Composite Structures
Author(s): Ramkumar, R. L. Corporate Author: Northrup Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1986-03-01 Report Number: AFWAL TR 86-3035
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Nonlinear Flying Quality Parameters Based on Dynamic Inversion
Author(s): Morton, B. G. Corporate Author: Honeywell Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-10-30 Report Number: AFWAL TR 87-3079
Experimental Modal Analysis and Dynamic Component Synthesis. Volume 1. Summary of Technical Work
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 1
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 2. Measurement Techniques for Experimental Modal Analysis
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 2
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 3. Modal Parameter Estimation
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 3
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 4. System Modeling Techniques
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 4
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 5. Universal File Formats
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 5
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Experimental Modal Analysis and Dynamic Component Synthesis. Volume 6. Software User's Guide
Author(s): Allenmang, Randall J. Corporate Author: University of Cincinnati Laboratory: Flight Dynamics Laboratory Date of Publication: 1987-12 Report Number: AFWAL TR 87-3069 Volume 6
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Evaluation of Lateral-Directional Handling Qualities and Roll-Sideslip Coupling of Fighter Class Airplanes
Author(s): Boothe, Edward M. Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y Laboratory: Flight Dynamics Laboratory Date of Publication: 1972-05 Report Number: AFFDL TR 72-36 Volume 1
Evaluation of Lateral-Directional Handling Qualities and Roll-Sideslip Coupling of Fighter Class Airplanes
Author(s): Boothe, Edward M. Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y Laboratory: Flight Dynamics Laboratory Date of Publication: 1972-05 Report Number: AFFDL TR 72-36 Volume 2
Strength, Efficiency, and Design Data for Beryllium Structures
Author(s): Crawford, Robert F. Corporate Author: Lockheed Missiles & Space Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: ASD TR 61-692
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Optimum Fatigue Spectra
Author(s): Neuls, G. S. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-04 Report Number: ASD TR 61-235
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Survey and Evaluation of Sonic Fatigue Testing Facilities
Author(s): Bianchi, Ralph A. Corporate Author: CONESCO Consultants in Engineering Science Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-03 Report Number: ASD TR 61-185 AD Number: AD0277124
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Fixed-Base Simulator Investigation of the Effect of L (sub alpha) and True Speed on Pilot Opinion of Longitudinal Flying Qualities
Author(s): Chalk, Charles R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-11 Report Number: ASD TDR 63-399
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Research on Techniques of Establishing Random Type Fatigue Curves for Broad Band Sonic Loading
Author(s): Fuller, J. R. Corporate Author: The Boeing Company, Transport Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: ASD TDR 62-501
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Inspection Periods Determined from Data of Crack Development and Strength Reduction of an Aircraft Structure Using Static Analysis
Author(s): Eggwertz, Sigge Corporate Author: The Aeronautical Research Institute of Sweden (FFA) Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-05 Report Number: ASD TDR 62-391
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Establishment of the Approach to, and Development of, Interim Design Criteria for Sonic Fatigue
Author(s): Fitch, G. E. Corporate Author: North American Aviation, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-06 Report Number: ASD TDR 62-26 AD Number: AD0284597
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Air Cushion Landing System Stability Study
Author(s): Burton, T. D. Corporate Author: Washington State University, Department of Mechanical Engineering Laboratory: Flight Dynamics Laboratory Date of Publication: 1980-11-01 Report Number: AFWAL TR 80-3150 AD Number: ADA097744
Calibration of an Axial Fan at Various Power Settings for Use on a Quarter Scale XC-8A Air Cushion Model
Author(s): Fischer, David L. Corporate Author: Mechanical Branch, Vehicle Equipment Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1980-01-01 Report Number: AFWAL TR 80-3094
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Superplastic Formed and Diffusion Bonded Titanium Landing Gear Component Feasibility Study
Author(s): Wilson, Vernon E. Corporate Author: Rockwell International, North American Aircraft Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1980-07-01 Report Number: AFWAL TR 80-3081
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Problems in Forced, Unsteady Fluid Mechanics
Author(s): Viets, Herman Corporate Author: Wright State University Laboratory: Flight Dynamics Laboratory Date of Publication: 1981-11-01 Report Number: AFWAL TM 81-148-FIMM
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Damping - A Key to More, Faster, Farther, Higher (Keynote Address)
Author(s): Ferguson, Thomas R., Jr. Corporate Author: Headquarters Air Force Systems Command Laboratory: Flight Dynamics Laboratory Date of Publication: 1989-11 Report Number: WRDC-TR-89-3116 Volume I p. AAA-1
Pioneering Damping in Space at GE Astro Space Division (Invited Speaker)
Author(s): Stahl, Clyde Corporate Author: GE Astro Space Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1989-11 Report Number: WRDC-TR-89-3116 Volume I p. AAB-1