Publication:
A method of characteristics approach to the problem of supersonic flow past oscillating cascades with finite blade thickness

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Authors
Vogeler, Konrad
Subjects
Unsteady Aerodynamics
Cascade Aerodynamics
Supersonic Blade Flutter
Aeroelasticity of Turbomachines
Method of Characteristics
Advisors
Date of Issue
1978-10
Date
1978-10
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
A method of characteristics approach is described for the computation of supersonic flow past oscillating cascades having blades of finite thickness distribution. The transonic small disturbance equation is solved for cascades with subsonic leading-edge locus. Sample calculations are presented for the inlet and passage flow and comparisons are given with calculations for flat-plate cascades and available measured pressure distributions. (Author)
Type
Technical Report
Description
Series/Report No
Department
Identifiers
NPS Report Number
NPS-67-78-012
Sponsors
Prepared for: Chief of Naval Research
Funder
Supported by the Office of the Naval Research through the Naval Postgraduate School Research Foundation Program
Format
xiii, 153 p. : ill. ; 28 cm.
Citation
Distribution Statement
Rights
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.
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