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Report Availability
82 reports
Integrated Information Presentation and Control System Study. Volume III. Degraded Mode Analysis.
Author(s): Premselaar, S. J. Corporate Author: Boeing Co Seattle Wash Military Aircraft Systems Div Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-06 Report Number: AFFDL TR 70-79 Volume 3
The "Paper Pilot" - A Digital Computer Program to Predict Pilot Rating for the Hover Task
Author(s): Dillow, James D. Corporate Author: Air Force Flight Dynamics Laboartory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-03 Report Number: AFFDL TR 70-40
Investigation of Measuring System Requirements for Instrument Low Visibility Approach
Author(s): Graham, Dunstan Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-02 Report Number: AFFDL TR 70-102
A Design Procedure and Handling-Quality Criteria for Lateral-Directional Flight Control Systems
Author(s): Stein, Gunter Corporate Author: Honeywell, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-05 Report Number: AFFDL TR 70-152
Validation of the Flying Qualities of MIL-F-008785A
Author(s): Brady, C. C. Corporate Author: McDonnell Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-01 Report Number: AFFDL TR 70-155
Background Information and User Guide for MIL-F-83300-Military Specification - Flying Qualities of Piloted V/STOL Aircraft
Author(s): Chalk, Charles R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-03 Report Number: AFFDL TR 70-88
A Theoretical Investigation of a Circular Lifting Jet in a Cross-Flowing Mainstream
Author(s): Hackett, J. E. Corporate Author: Lockheed-Georgia Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-01 Report Number: AFFDL TR 70-170
Precision Attitude Control of Symmetric Spinning Bodies
Author(s): Lorell, Kenneth R. Corporate Author: Stanford University Department of Aeronautics and Astronautics Laboratory: Air Force Avionics Laboratory Date of Publication: 1971-04 Report Number: AFAL TR 71-224
Doppler Aided Strapdown Inertial Flight Test Program - 1971
Author(s): Pearson, Vance H. Corporate Author: Honneywell Inc, St. Petersburg, Florida Laboratory: Air Force Avionics Laboratory Date of Publication: 1971-12 Report Number: AFAL TR 71-368
Solid Lubricated Bearing Technology. Part I. Solid Lubricated High Speed Ball Bearing
Author(s): Boes, D. J. Corporate Author: Wetinghouse Research Labs, Pittsburgh, Pennsylvania Laboratory: Air Force Aero Propulsion Laboratory Date of Publication: 1971-08 Report Number: AFAPL TR 71-69 Part 1
Study of Folding Proprotor VTOL Aircraft Dynamics. Volume I. Analytical Methods.
Author(s): Yen, Jing G. Corporate Author: Bell Helicpter Textron Inc., Fort Worth, Texas Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-09 Report Number: AFFDL TR 71-7 Volume 1
Statistical Analysis of LO-LOCAT Turbulence Data for Use in the Development of Revised Gust Criteria
Author(s): McCloskey, John W. Corporate Author: Dayton University Research Institute Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-04 Report Number: AFFDL TR 71-29
Theory of an Air Cushion Landing System for Aircraft
Author(s): Digges, Kennerly H. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-06 Report Number: AFFDL TR 71-50
Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume II. Component Design Studies.
Author(s): Fry, Bernard L. Corporate Author: Boeing Vertol Company, Philadelphia, Pennsylvania Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-07 Report Number: AFFDL TR 71-62 Volume 2
New Techniques in Nondestructive Testing (Exo-Electron Emission Phase). Part I.
Date of Publication: 1971-12 Report Number: AFML TR 71-140
full text by request
AFML Torsional Split Hopkinson Bar
Date of Publication: 1971-07 Report Number: AFML TR 71-145
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Development of a High Speed Biaxial Testing Machine
Date of Publication: 1971-07 Report Number: AFML TR 71-149
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Analytical Study of the Split Hopkinson Bar Technique for Strain-Rate Dependent Material Behavior
Date of Publication: 1971-08 Report Number: AFML TR 71-155
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Development and Applications of Nondestructive Methods for Predicting Mechanical Properties of Advanced Reinforced Nonmetallic Composites.
Date of Publication: 1971-09 Report Number: AFML TR 71-168
full text by request
Fine Subgrain Structure Adjacent to Fatigue Cracks
Date of Publication: 1971-10 Report Number: AFML TR 71-211
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New and Refined Nondestructive Techniques for Graphite Billets and Shapes
Author(s): Oaks, A. E. Corporate Author: General Electric Company Laboratory: Air Force Materials Laboratory Date of Publication: 1971-07 Report Number: AFML TR 70-212 Part 2
full text by request
Eddy Current Inspection of Turbine Blades
Date of Publication: 1971-10 Report Number: AFML TR 70-266
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Flammability and Heat Transfer Characteristics of PBI Fabric
Date of Publication: 1971-01 Report Number: AFML TR 70-267
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The Development and Use of a Torsional Split Hopkinson Bar for Experiments in Dynamic Plasticity
Date of Publication: 1971-05 Report Number: AFML TR 71-32
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Effect of Strain Rate, Temperature and Multiaxial Stress on the Strength and Ductility of S-200E Beryllium and 6Al-4V Titanium
Date of Publication: 1971-03 Report Number: AFML TR 71-37
full text by request
Study of Deformation and Defects Occurrence in Advanced Forging Technique
Date of Publication: 1971-09 Report Number: AFML TR 71-69
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Failure Mechanism of Attitude Control System Valve in Chlorine Pentafluoride Service
Date of Publication: 1971-07 Report Number: AFML TR 71-94
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Comparison of Major Forging Systems
Author(s): Lake, Frank N. Corporate Author: TRW Inc. Laboratory: Air Force Materials Laboratory Date of Publication: 1971-05 Report Number: AFML TR 71-112
Investigation of Pilots' Tracking Capability Using a Roll Command Display
Author(s): Gieselhart, Richard Corporate Author: Aeronautical Systems Division Laboratory: Aeronautical Systems Division Date of Publication: 1971-12 Report Number: ASD TR 71-46
Survivable Flight Control System Interim Report No. 1 Studies, Analyses and Approach: Supplement for Hydraulic Power and Actuation Studies
Author(s): Amies, Gerald E. Corporate Author: McDonnell Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-05 Report Number: AFFDL TR 71-20 Supplement 3
Validation of the Flying Qualities Requirements of MIL-F-8785B (ASG)
Author(s): Kandalft, R. N. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-09 Report Number: AFFDL TR 71-134
Total In-Flight Simulator (TIFS) - Preliminary Design Report
Author(s): Arendt, R. H. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-08 Report Number: AFFDL TR 71-119
In-Flight Test Results on Mission-Oriented Cockpit Lighting Requirements
Author(s): DeBruine, C. J. Corporate Author: Lear Siegler, Inc.; North American Rockwell Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-09 Report Number: AFFDL TR 71-142
Survivable Flight Control System Interim Report No. 1: Studies, Analyses and Approach
Author(s): Hooker, David S. Corporate Author: McDonnell Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-05 Report Number: AFFDL TR 71-20
Survivable Flight Control System Interim Report No. 1 Studies, Analyses, and Approach: Supplement for Control Law Development Studies
Author(s): Kisslinger, Robert L. Corporate Author: McDonnell Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-05 Report Number: AFFDL TR 71-20 Supplement 2
Preliminary Handling Qualities Requirements for Lifting Re-Entry Vehicles During Terminal Flight
Author(s): Di Franco, Dante A. Corporate Author: Corenell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-08 Report Number: AFFDL TR 71-64
The Generation of a Military Specification for Flying Qualities of Piloted V/STOL Aircraft - MIKL-F-83300
Author(s): Key, David L. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-03 Report Number: AFFDL TR 71-23
Survivable Flight Control System Interim Report No. 1 Studies, Analyses and Approach: Supplement for Control Criteria Studies
Author(s): Kisslinger, Robert L. Corporate Author: McDonnell Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-05 Report Number: AFFDL TR 71-20 Supplement 1
Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume III - Appendixes
Author(s): Fry, Bernard L. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-07 Report Number: AFFDL TR 71-62 Volume 3
Volume IV. Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part I. Analysis and Results
Author(s): Magee, John Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-08 Report Number: AFFDL TR 71-62 Volume 4 Part 1
Volume V. Wind Tunnel Test of a Powered Tilt-Rotor Perfromance Model
Author(s): Magee, John P. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-62 Volume 5
Volume VI. Wind Tunnel Test of a Powered Tilt-Rotor Dynamic Model on a Simulated Free Flight Suspension System
Author(s): Tomassoni, John E. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-62 Volume 6
Volume VII. Wind Tunnel est of the Aerodynamics and Dynamics of Rotor Spinup, Stopping and Folding on a Semispan Folding Tilt-Rotor Model
Author(s): van Wagensveld, Dirk Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-62 Volume 7
Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume IX. Value Engineering Report
Author(s): Liiva, Jaan Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-62 Volume 9
Analysis of Structural Shells with Transverse Shear Deformation
Author(s): Citerley, Richard L. Corporate Author: Anamet Laboratories, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-11 Report Number: AFFDL TR 71-116
Fabrication and Instrumentation of an Experimental Passive Radiative Infrared Detector Cooler for Spacecraft Applications
Author(s): Schmidt, W. F. Corporate Author: Philco-Ford Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-125
Volume IV. Wind Tunnel Test of the Concersion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part II. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details
Author(s): Magee, John Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-08 Report Number: AFFDL TR 71-62 Volume 4 Part 2
Method for the Prediction of Performance of STOL High Lift Systems Near Maximum Lift Coefficient
Author(s): Bauer, Paul T. Corporate Author: University of Dayton Research Institute Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-12 Report Number: AFFDL TR 71-169
Preliminary Design Study for an Advanced Fighter Type In-Flight Simulator
Author(s): Gallagher, J. T. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-10 Report Number: AFFDL TR 71-149
full text by request
Investigation of Measuring System Requirements for Low Visibility Landing
Author(s): Hofmann, Lee Gregor Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1971-12 Report Number: AFFDL TR 71-151