Centrifugal stress in conical rotors and rotors of arbitrary cross section
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Author
Harshberger, Robert Lee
Troutman, Darrell Clinton
Date
1966-05Advisor
Gawain, Theodore H.
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Show full item recordAbstract
Part I of this report evaluates a computer solution for
the centrifugal stresses in rotors of arbitrary cross section,
as proposed by Lt. R. A. Johnson in 1965- This solution was
found to be unstable and in its present form is unacceptable.
Part II is an evaluation of the hot spin test unit of
the United States Naval Postgraduate School. This facility was found capable of measuring centrifugal strains with
excellent accuracy. Part III presents a new and original analytical solution
for the stresses in any conical rotor of constant thickness.
The theoretically predicted stresses are found to be in close
agreement with the measured values for the particular rotor
tested.
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This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.Collections
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