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- 1966 (94)
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94 reports
Theoretical Investigations of Boundary Layer Stability
Author(s): Raetz, Gibbs S. Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 64-184
Estimation of Flying Qualities of Piloted Airplanes
Author(s): Woodcock, Robert J. Corporate Author: Douglas Aircraft Co. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 65-218
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): Nielsen, Jack N. Corporate Author: Itek Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-107 Part 2
The Light-Line-Tethering Technique for Determining the Aerodynamic Derivatives of an Air Cushion Vehicle
Author(s): Kurylowich, G. Corporate Author: University of Toronto Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 65-159
Simulated Landing Approaches of an Unaugmented C-5A Configuration
Author(s): Newell, F. D. Corporate Author: Cornell Aeronautical Laboratories Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-03 Report Number: AFFDL TR 65-210
Statics and Stability of Thin-Walled Elastic Beams: Part I. Formulation of Fundamental Equations
Author(s): Giangreco, E. Corporate Author: University of Naples Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-213 Part 1
Compilation and Analysis of Flight Control System Command Inputs
Author(s): Weir, David H. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-119
Investigations of Describing Function Technique
Author(s): Graham, Dunstan Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-02 Report Number: AFFDL TR 65-137
Experimental Program to Determine Effect of Crack Buckling and Specimen Dimensions on Fracture Toughness of Thin Sheet Materials
Author(s): Forman, R. G. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-146
Titan III 20 Percent Dynamic Model Characteristics - Comparison of Theory and Experiment
Author(s): Morosow, George Corporate Author: Martin Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 945-973
A Closed-Form Solution to Lifting Reentry
Author(s): Bell, Roland N. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-01 Report Number: AFFDL TR 65-65
Pressure Distribution During Parachute Opening. Phase 1. Infinite Mass Operating Case
Author(s): Melzig, H. D. Corporate Author: Deutsche Forschungsanstalt Fuer Luft- Und Raumfahrt E V Brunswick (Germany Fr) Inst Fuer Flugmechanik Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-03 Report Number: AFFDL TR 66-10
Analysis And Experimental Evaluation Of An Ultra-High Temperature Pyrolytic Graphite Thermocouple
Author(s): Klein, C. A. Corporate Author: Raytheon Co Waltham Ma Research Div Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 66-27
Investigation Of Space Package Alightment Dynamic Load Design Criteria
Author(s): York, K. C. Corporate Author: General Dynamics Corp Pomona Ca Pomona Div Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-33
Investigation Of Friction, Wear And Failure In Aerospace Bearings
Author(s): Staph, H. E. Corporate Author: Southwest Research Inst San Antonio TX Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-75
Aerodynamic Noise Simulation In Sonic Fatigue Facility
Author(s): Lyon, R. H. Corporate Author: Bolt Beranek And Newman Inc Cambridge Mass Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL TR 66-112
Measurement And Analyses Of The J57-P21 Noise Field
Author(s): Hermes, P. H. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-147
Solid-State Display Devices
Author(s): Van Winkle, Glen Corporate Author: Lear Siegler, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-81
A Prototype Peripheral Vision Aircraft Attitude Display
Author(s): Williamson, William R. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-91
Effects of Manipulator Restraints on Human Operator Performance
Author(s): Magdaleno, R. E. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-12 Report Number: AFFDL TR 66-72
Development of High Contrast Electroluminescent Techniques for Aircraft Displays
Author(s): Peterson, Carlton J. Corporate Author: Bunker-Ramo Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-6
Human Pilot Dynamic Response in Single-Loop Systems with Compensatory and Pursuit Displays
Author(s): Wasicko, R. J. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-12 Report Number: AFFDL TR 66-137
Human Pilot Dynamics with Various Manipulators
Author(s): McRuer, D. T. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-12 Report Number: AFFDL TR 66-138
Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack
Author(s): Nagel, A. L. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-122
Flight Evaluation of Various Phugoid Dynamics and 1/Th1 Values for the Landing Approach Task
Author(s): Chalk, Charles Corporate Author: Cornell Aeronutical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-02 Report Number: AFFDL TR 66-2
Re-Entry Vehicle Control System Design and Mechanization
Author(s): Scharmack, D. K. Corporate Author: Honeywell, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-3
Low Pressure Measurement Techniques
Author(s): Painter, Herbert A. Corporate Author: Electro-Optical Systems, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-11
Stiffness and Vibration Characteristics of Inflatable Delta Wing Models at Temperatures up to 650°F
Author(s): Pollock, Samuel J. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 66-14
Mathematical Analysis of Heat Conduction in a Sector of a Hollow Circular Cylinder
Author(s): None Given Corporate Author: Martin Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-16
Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Author(s): Achard, Robert T. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-25
Methods of Calculating Aerodynamic Loads on Aircraft Structures: Part I - Wing-Body Interference Effects
Author(s): Borland, Christopher J. Corporate Author: Massachusetts Institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-37 Part 1
Methods of Calculating Aerodynamic Loads on Aircraft Structures: Part II - Nonlinear Effects
Author(s): Chamberlain, Thomas E. Corporate Author: Massachusetts Institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-37 Part 2
Methods of Calculating Aerodynamic Loads on Aircraft Structures: Part III - Effects of Engines, Stores and Wing-Tail Interference
Author(s): Chou, David C. Corporate Author: Massachusetts Institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-37 Part 3
Aircraft Ground-Flotation Investigation: Part II - Data Report on Test Section 1
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-43 Part 2
Aircraft Ground-Flotation Investigation: Part III - Data Report on Test Section 2
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-43 Part 3
Aircraft Ground-Flotation Investigation: Part V - Data Report on Test Section 4
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 5
Aircraft Ground-Flotation Investigation: Part VII - Data Report on Test Section 6
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 7
Aircraft Ground-Flotation Investigation: Part VIII - Data Report on Test Section 7
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 8
Aircraft Ground-Flotation Investigation: Part IX - Data Report on Test Section 8
Author(s): Rutledge, A. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 9
Aircraft Ground-Flotation Investigation: Part X - Data Report on Test Section 9
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 10
Aircraft Ground-Flotation Investigation: Part XI - Data Report on Test Section 10
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 11
Aircraft Ground-Flotation Investigation: Part XII - Data Report on Test Section 12
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 12
Aircraft Ground-Flotation Investigation: Part XIII - Data Report on Test Section 13
Author(s): Watkins, J. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-43 Part 13
Aircraft Ground-Flotation Investigation: Part XIV - Data Report on Test Section 14
Author(s): Watkins, J. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 14
KC-135 Power Spectral Vertical Gust Load Analysis: Volume II - Supplemt Results
Author(s): Latz, Robert N. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-57 Volume 2
Preliminary Development of Gust Design Procedures Based on Power Spectral Techniques: Volume I - Theoretical and General Considerations
Author(s): Houbolt, John C. Corporate Author: Aeronautical Research Associates of Princeton, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-58 Volume 1
Preliminary Development of Gust Design Procedures Based on Power Spectral Techniques: Volume II - Summary of Possible Procedures
Author(s): Houbolt, John C. Corporate Author: Aeronautical Research Associates of Princeton, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-58 Volume 2
Approximate Structural Analysis Techniques Employing Undetermined Parameters
Author(s): Ojalvo, I. U. Corporate Author: Fairchild Hiller Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-59
Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results
Author(s): Hayes, J. A. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-12 Report Number: AFFDL TR 66-78
Design Calculations on Proven Trainer and Fighter Aircraft for the Verification of a Gust Design Procedure
Author(s): Hwang, Chintsun Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-82