Theory of aeroplane structural members subjected to combined axial and non-uniform transverse loads
By: by John Elliott Younger.
Publisher: University of California press
Published: 1926
Place of publication: [Berkeley, Calif
Language: eng
Number of pages: 275
Subjects: Airplanes.; Strains and stresses.
Notes: Bibliography: p. 275.
Thesis (Ph. D.)--University of California, 1925.
University of California publications in engineering, v. 2, no. 8, with a special thesis t.-p. attached to the cover.