The torsional stiffness of thin duralumin shells subjected to large torques (1934)
NASA Technical Reports Server (NTRS) · leaf 14
N.A.C.A. Teennloal Hot* Ho.500 *iga. 12,13 … .004 .008 .013 .016 .030 .024 .028 8, radian Tig.13.- Computed 80,000 and ex- peri- mental values of vari- ation ,0 60,000 of angle of twist with torque for a wing panel. g40,000 Experi- E-i mental data from refer- ence 5. 20,000 Twist was measured between ribs 2 and 7 10 40 SO 60 70 6, radian
NASA Technical Reports Server (NTRS)
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