Two‐Spar Wing Stress Analysis

  • A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen
  • W.J. Goodey
  • Aircraft Engineering and Aerospace Technology, October 1949, Emerald
  • DOI: 10.1108/eb031816

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http://dx.doi.org/10.1108/eb031816

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