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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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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): DeGroff, Harold M.
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 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): Williams, M. L., Garrett, J., Henry, W. E.
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 7
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 9. On the Stresses in Cantilever Plates of Arbitrary Planform and Variable Thickness (A Relaxation Procedure With Applications to the Swept Wing Problem)
Author(s): Fung, Y. C.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Report number: AF TR 5761 Part 9
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:
Author(s): Sechler, E. E., Dixon, H. H.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-12-01
Report number: AF TR 5761 Part 13

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