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
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Report Number: AF TR 5761 Part 11
Author(s): Williams, M. L., Hrebec, G. M.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Pages: 70
Contract: W33-038-ac-16961
DoD Task:
Identifier: AD0091384
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Author(s): Williams, M. L., Hrebec, G. M.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Pages: 70
Contract: W33-038-ac-16961
DoD Task:
Identifier: AD0091384
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero