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Eye Fixations of Aircraft Pilots, IV. Frequency, Duration, and Sequence of Fixations During Routine Instrument Flight
Author(s): Jones, Richard E., Fitts, Paul M., Milton, John L.
Corporate Author(s): Wright-Patterson Air Force Base
Laboratory: Air Materiel Command
Date of Publication: 1949-12
Report number: AF TR 5975
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Eye Fixations of Aircraft Pilots. III. Frequency, Duration, and Sequence Fixations When Flying Air Force Ground-Controlled Approach System
Author(s): Fitts, Paul M., Milton, John L., Jones, Richard E.
Corporate Author(s): Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 1949-11
Report number: AF TR 5967
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Eye Fixations of Aircraft Pilots, II. Frequency, Duration, and Sequence of Fixations When Flying the USAF Instrument Low Approach System (ILAS)
Author(s): Milton, John L., Fitts, Paul M., Jones, Richard E.
Corporate Author(s): Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 1949-10
Report number: AF TR 5839
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Eye Fixations of Aircraft Pilots I. A Review of Prior Eye-Movement Studies and a Description of a Techniques for Recording the Frequency, Duration, and Sequences of Eye Fixations During Instrument Flight
Author(s): Jones, Richard E., Fitts, Paul M., Milton, John L.
Corporate Author(s): Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 1949-09
Report number: AF TR 5837
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Fundamental Characteristics of High Performance Hydraulic Systems
Author(s): Campbell, James E.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Materiel Command
Date of Publication: 1950-06
Report number: AF TR 5997
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 12. On the Stresses and Deflection of Swept Thick-Walled Box Beams
Author(s): Fung, Y. C.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Report number: AF TR 5761 Part 12
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 11. An Experimental Investigation of Stresses and Deflections in a Swept Thick-Walled Box Beam
Author(s): Williams, M. L., Hrebec, G. M.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Report number: AF TR 5761 Part 11
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 14. Errata and Revisions
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-11-01
Report number: AF TR 5761 Part 14
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 4. Application of the Electric Analog Computer to the Elastic Plate Problem
Author(s): MacNeal, Richard H.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Report number: AF TR 5761 Part 4
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 6. The Plate Problem for a Cantilever Sector of Uniform Thickness
Author(s): Williams, M. L.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-11-01
Report number: AF TR 5761 Part 6

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