United States. National Advisory Committee for Aeronautics. (1939). Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression. [s.n.].
Chicago Style (17th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Stability of Rectangular Plates with Longitudinal or Transverse Stiffeners Under Uniform Compression. [Washington]: [s.n.], 1939.
MLA (9th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Stability of Rectangular Plates with Longitudinal or Transverse Stiffeners Under Uniform Compression. [s.n.], 1939.
Warning: These citations may not always be 100% accurate.