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article · Aircraft Engineering and Aerospace Technology · 1939

Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening

E.J. Richards

Cited by 1Abstract and details only

Abstract

A GENERAL solution is obtained for the diffusion of stress in n equal and equally spaced stringers in a stiffened panel subject to any boundary conditions at the ends of the stringers.

Cite this paper

APA 7

Richards, E. (1939). Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening. Aircraft Engineering and Aerospace Technology, 11(8), 301–305. https://doi.org/10.1108/eb030524

MLA 9

Richards, E.J. “Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening.” Aircraft Engineering and Aerospace Technology, vol. 11, no. 8, 1939, pp. 301–05, https://doi.org/10.1108/eb030524.

Chicago

Richards, E.J. 1939. “Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening.” Aircraft Engineering and Aerospace Technology 11 (8): 301–05. https://doi.org/10.1108/eb030524.

Harvard

Richards, E. (1939) ‘Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening’, Aircraft Engineering and Aerospace Technology, 11(8), pp. 301–305. Available at: https://doi.org/10.1108/eb030524.

BibTeX
@article{richards1939transfer,
  title = {{Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening}},
  author = {Richards, E.J.},
  journal = {Aircraft Engineering and Aerospace Technology},
  volume = {11},
  number = {8},
  pages = {301--305},
  year = {1939},
  doi = {10.1108/eb030524}
}

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