Creep Buckling of Relatively Thick Circular Cylindrical Shells Compressed Axially
Download or Read eBook Creep Buckling of Relatively Thick Circular Cylindrical Shells Compressed Axially PDF written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1973 with total page 34 pages. Available in PDF, EPUB and Kindle.
Author | : Stanford University. Department of Aeronautics and Astronautics |
Publisher | : |
Total Pages | : 34 |
Release | : 1973 |
ISBN-10 | : STANFORD:36105046321373 |
ISBN-13 | : |
Rating | : 4/5 (73 Downloads) |
Book Synopsis Creep Buckling of Relatively Thick Circular Cylindrical Shells Compressed Axially by : Stanford University. Department of Aeronautics and Astronautics
Book excerpt: Experimental results obtained with 31 nickel circular cylindrical shell specimens are evaluated in the light of the theory. The test results have already been reported in SUDAAR No. 415. The experimental creep buckling times obtained in axial compression at a temperature of 650F were found to be in reasonable agreement with the theoretical formulas. (Author).