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100 items
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Development of High Contrast Electroluminescent Techniques for Aircraft Displays
Author(s): Peterson, Carlton J., Smith, Hugh A.Corporate Author(s): Bunker-Ramo Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-6
full text available
Human Pilot Dynamic Response in Single-Loop Systems with Compensatory and Pursuit Displays
Author(s): Wasicko, R. J., McRuer, D. T., Magdaleno, R. E.Corporate Author(s): Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-12
Report number: AFFDL TR 66-137
full text available
Human Pilot Dynamics with Various Manipulators
Author(s): McRuer, D. T., Magdaleno, R. E.Corporate Author(s): Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-12
Report number: AFFDL TR 66-138
full text available
Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack
Author(s): Nagel, A. L., Savage, R. T., Wanner, R., Blank, R. W.Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-08
Report number: AFFDL TR 66-122
full text available
Flight Evaluation of Various Phugoid Dynamics and 1/Th1 Values for the Landing Approach Task
Author(s): Chalk, CharlesCorporate Author(s): Cornell Aeronutical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-02
Report number: AFFDL TR 66-2
full text available
Re-Entry Vehicle Control System Design and Mechanization
Author(s): Scharmack, D. K., Ward, M. D.Corporate Author(s): Honeywell, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-3
full text available
Low Pressure Measurement Techniques
Author(s): Painter, Herbert A.Corporate Author(s): Electro-Optical Systems, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-07
Report number: AFFDL TR 66-11
full text available
Stiffness and Vibration Characteristics of Inflatable Delta Wing Models at Temperatures up to 650°F
Author(s): Pollock, Samuel J.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-06
Report number: AFFDL TR 66-14
full text available
Mathematical Analysis of Heat Conduction in a Sector of a Hollow Circular Cylinder
Author(s): None GivenCorporate Author(s): Martin Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-16
full text available
Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Author(s): Achard, Robert T.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Report number: AFFDL TR 66-25
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