An investigation of the flow in turbojet test cell augmenters.
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Authors
Hayes, Jack Douglas
Subjects
turbojet test cell
Advisors
Netzer, David W.
Date of Issue
1975-09
Date
September 1975
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
A two-dimensional elliptic computer model was adapted to the solution of the flow field in a turbojet thest cell section which contained the engine exhaust duct and augmenter tube. Various engine power settings, augmentation ratios, and augmenter geometries were investigated. Flow visualization and static pressure recovery were primary objectives subject to specified engine power settings and augmentation ratios. Capabilities and limitations of the model are discussed.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Naval Air Propulsion Test Center N6237675WR00037
Funder
Naval Air Propulsion Test Center N6237675WR00037
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
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.