Some elementary principles of shell stress analysis with notes on the use of the shear center (1939)
NASA Technical Reports Server (NTRS) · leaf 18
As example, the equation for--the simple case of figure 11 will be developed. ST: P + Sx - S8 = 0 ' (a) ZM: -Fd + S3h + Saw = 0 (b) s s SL on flange li dlS + -r~ dz - — dz = 0 (c) n w S S SL on flange 2: dP2 + -~ dz - dz = 0 (d)
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
