Procedure for case of simultaneous change of moment of inertia, change of distributed load, and concentrated load at point in main bay. (supp.)
Graphical method of stressing aeroplane spars
Flight
Flight ; 23 , n 17 ; p 362a-362c
1931
7 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
New method of stressing wooden spars
Engineering Index Backfile | 1935
|Stressing of aeroplane wings due to symmetrical gusts
TIBKAT | 1936
|Strength of aeroplane wing spars with end loads varying in any one bay
Engineering Index Backfile | 1934
|