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

The authors haven't yet claimed this publication.

Read Publication

In partnership with: