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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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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): Hrebec, G. M.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 8
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