United States. National Advisory Committee for Aeronautics. (1939). Limit of stability of curved plate strip under shear and axial stresses. [s.n.].
Chicago Style (17th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Limit of Stability of Curved Plate Strip Under Shear and Axial Stresses. [Washington]: [s.n.], 1939.
MLA (9th ed.) CitationUnited States. National Advisory Committee for Aeronautics. Limit of Stability of Curved Plate Strip Under Shear and Axial Stresses. [s.n.], 1939.
Warning: These citations may not always be 100% accurate.