Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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Laboratory

17 reports

Eye Fixations of Aircraft Pilots, IV. Frequency, Duration, and Sequence of Fixations During Routine Instrument Flight

Author(s): Richard E. Jones; John L. Milton, Paul M. Fitts
Corporate Author: Wright-Patterson Air Force Base
Laboratory: Air Materiel Command
Date of Publication: 12/1/1949
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): Paul M. Fitts; Richard E. Jones; John L. Milton
Corporate Author: Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 11/1/1949
Report Number: AF TR 5967
full text available

Eye Fixations of Aircraft Pilots, II. Frequency, Duration, and Sequence of Fixations When Flying the USAF Instrument Low Approach System (ILAS)

Author(s): John L. Milton; Richard E. Jones; Paul M. Fitts
Corporate Author: Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 10/1/1949
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.; Milton, John L.; Fitts, Paul M.
Corporate Author: Air Materiel Command
Laboratory: Air Materiel Command
Date of Publication: 9/1/1949
Report Number: AF TR 5837
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Fundamental Characteristics of High Performance Hydraulic Systems

Author(s): James E. Campbell
Corporate Author: North American Aviation, Inc.
Laboratory: Air Materiel Command
Date of Publication: 6/1/1950
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): Y. C. Fung
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 9/1/1950
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): M. L. Williams; G. M. Hrebec
Corporate Author: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 9/1/1950
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: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 11/1/1950
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): Richard H. MacNeal
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 10/1/1950
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): M. L. Williams
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 11/1/1950
Report Number: AF TR 5761 Part 6
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 3. Experimental Investigation of the Effect of Sweep Upon the Stress and Deflection Distribution in Cantilever Plates of Constant Chord and Thickness

Author(s): Harold M. DeGroff
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 10/1/1950
Report Number: AF TR 5761 Part 3
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 7. An Experimental Investigation of the Stresses and Deflections in a Series of Cantilever Sectors of Uniform Thickness

Author(s): M. L. Williams; J. Garrett; W. E. Henry
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 11/1/1950
Report Number: AF TR 5761 Part 7
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:

Author(s): E. E. Sechler; H. H. Dixon
Corporate Author: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 12/1/1950
Report Number: AF TR 5761 Part 13
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"Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity" Part I - "Elastostatic and Aeroelastic Problems Relating to Thin Wings of High-Speed Airplanes"

Author(s): Yuan-Cheng Fung
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 2/1/1949
Report Number: AF TR 5761 Part 1
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Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 2. Stress and Deflection Analysis of Swept Plates

Author(s): Yung-Cheng Fung
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 12/1/1949
Report Number: AF TR 5761 Part 2
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 8. Some Experimental Data on the Deflection and Root Stresses in a Cantilever Triangular Plate of Constant Thickness With Varying Trailing Edge Sweep Angle

Author(s): G. M. Hrebec
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 11/1/1950
Report Number: AF TR 5761 Part 8
full text unavailable