13 reports
Fundamental Characteristics of High Performance Hydraulic Systems
Author(s): Campbell, James E. Corporate Author: North American Aviation, Inc. Laboratory: Air Materiel Command Date of Publication: 1950-06 Report Number: AF TR 5997
full text unavailable
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: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-09-01 Report Number: AF TR 5761 Part 12
full text unavailable
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. Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 1950-09-01 Report Number: AF TR 5761 Part 11
full text unavailable
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
full text unavailable
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: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-10-01 Report Number: AF TR 5761 Part 4
full text unavailable
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: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-11-01 Report Number: AF TR 5761 Part 6
full text unavailable
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: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-10-01 Report Number: AF TR 5761 Part 3
full text unavailable
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. 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
full text unavailable
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: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 1950-10-01 Report Number: AF TR 5761 Part 9
full text unavailable
Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:
Author(s): Sechler, E. E. Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 1950-12-01 Report Number: AF TR 5761 Part 13
full text unavailable
"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): Fung, Yuan-Cheng 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
full text unavailable
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): Fung, Yung-Cheng 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
full text unavailable
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: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-11-01 Report Number: AF TR 5761 Part 8
full text unavailable