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: 1950-11-01
Report Number: AF TR 5761 Part 8

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: 1949-12-01
Report Number: AF TR 5761 Part 2

"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: 1949-02-01
Report Number: AF TR 5761 Part 1

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): Y. C. Fung
Corporate Author: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Report Number: AF TR 5761 Part 9

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: 1950-11-01
Report Number: AF TR 5761 Part 7

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: 1950-10-01
Report Number: AF TR 5761 Part 3

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: 1950-11-01
Report Number: AF TR 5761 Part 6

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: 1950-10-01
Report Number: AF TR 5761 Part 4

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: 1950-11-01
Report Number: AF TR 5761 Part 14

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: 1950-09-01
Report Number: AF TR 5761 Part 11

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: 1950-09-01
Report Number: AF TR 5761 Part 12

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: 1950-12-01
Report Number: AF TR 5761 Part 13

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: 1950-06
Report Number: AF TR 5997