Results obtained at high values of internal pressure differ from those obtained previously in that theoretical small-deflection compressive buckling coefficient of 0.6 was nearly achieved in each test; small amounts of internal pressure had greater stabilizing effect in bending than in compression tests; pertinence to fuselage for aircraft or missiles if expected air- and maneuver-loads are small.
Bending and compression tests of pressurized ring-stiffened cylinders
NASA -- Tech Note
1960
27 pages
Report
English
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