The buckling in compression of panels with square top-hat section stringers / by W.S. Hemp and K.H. Griffin ; communicated by E.F.. Relf.
Aircraft design; Aircraft structures; Buckling; Compressive strength; Panels; Stiffening; Stringers; Structural design; ; Compression loads; Fabrication; Structural analysis; Structural failure.
Saved in:
Main Author: | |
---|---|
Corporate Author: | |
Other Authors: | |
Format: | Book |
Language: | English |
Published: |
London :
H.M.S.O.,
Between 1950 and [1959?]
|
Series: | Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
no. 2635. |
Subjects: |