An empirical method of determining the crippling stress for flanged frames of Alclad 24 S-T at room temperature and elevated temperature
By: Gunnar Anevi.
Contributors: Saab Aircraft Company
Series: Saab Aircraft Company. Technical notes -- 40
Publisher: Saab Aircraft Company
Published: 1958
Place of publication: Linkoping, Sweden
Number of pages: 24
Notes: Bibliography: p. 9.