Zobrazeno 1 - 2
of 2
pro vyhledávání: '"M. L. Parin"'
Publikováno v:
Volume 1B: Gas Turbines.
Welded titanium inlet guide vanes in an Air Force turbojet engine, have been experiencing a high rate of vibration induced cracking after very short service The cause of this cracking has been identified as resonant vibration excited by pressure fluc
Publikováno v:
Volume 1A: General.
A finite-element analysis utilizing isoparametric elements is used to predict the modal damping and resonant frequencies of a jet engine high pressure compressor stator vane with a damping treatment in the form of an enamel coating applied to the sur