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
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
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
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.
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.
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.
@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}
}Made from the index record. Check names, capitalisation and page numbers against the paper. Need another style? AI for Research has over 10,000.
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