A primitive variable mathematical model for predicting the flows in turbojet test cells

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Authors
Stevenson, Charles A.
Netzer, David W.
Subjects
Turbojet Test Cells
Computer Model
Advisors
Date of Issue
1979-10
Date
1979-10
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
An adaptation of a primitive variable, finite-difference computer program was made in order to predict the non-reacting flow fields in turbojet test cells. The study compares the predictions of the primitive variable computer model with an earlier stream function-vorticity computer model and empirical data. It was found that the model reasonably predicted the flow fields and allowed simulation of test cell flows up to full engine throttle conditions
Type
Technical Report
Description
URI
https://hdl.handle.net/10945/29046
Series/Report No
Department
Organization
Graduate School of Operational and Information Sciences (GSOIS)
Identifiers
NPS Report Number
NPS67-79-009
Sponsors
Prepared for: Naval Air Propulsion Center, Trenton, NJ.
Funder
N6237679WR00014
Format
xiii, 61 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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