Blade-forced vibration effects in turbomachinery rotor-stator interaction
Date
2000
Authors
Journal Title
Journal ISSN
Volume Title
Publisher
Texas A&M University
Abstract
This thesis presents the effects of blade-forced vibration in turbomachinery rotor-stator interaction. A quasi-three-dimensional multi-row analysis, based on an Euler/Navier-Stokes solver and a parallel computational algorithm, was used to simulate the unsteady flow in a turbine. Results are presented for non-dimensional pressure, velocity, and entropy in the blade passage. The two-stage turbine flow analysis was completed for the case with blade-forced response as well as the case without blade-forced response for comparison.
Description
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Includes bibliographical references (leaves 58-62).
Issued also on microfiche from Lange Micrographics.
Includes bibliographical references (leaves 58-62).
Issued also on microfiche from Lange Micrographics.
Keywords
aerospace engineering., Major aerospace engineering.