Basava Raju, B and Chandra, R (1976) Some experiments on buckling of electroformed nickel shell specimens. Journal of Aeronautical Society of India, 28 . pp. 59-67.Full text not available from this repository.
A controlled end-displacement type test rig was developed to study the buckling of electroformed thin circular cylindrical nickel shell specimens; to measure the stress distribution around the shell, a straingage type of load cell was devised. Experimental values of buckling load approximated 65% of the classical values, while the typical load variation around the circumference of the shell was found to be about 15%.
|Item Type:||Journal Article|
|Uncontrolled Keywords:||Buckling;Cylindrical shells;Electroforming;Load testing; Machines;Metal shells;Nickel;Circular cylinders;Shell stability;Thin walled shells|
|Subjects:||AERONAUTICS > Aeronautics (General)|
|Division/Department:||Structures Division, Structures Division|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||04 Jan 2007|
|Last Modified:||01 Sep 2015 14:26|
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