Internal Aerodynamics of Turbojet Test Cells
Author
Speakman, G. C.
Hayes, J. D.
Netzer, D. W.
Date
1976-12Second Reader
Bell, R. W.
Metadata
Show full item recordAbstract
Elliptic computer codes have been developed (including plot routines) which can be used to study the flow field in test cells and exhaust stacks and in the augmenter tube for low thrust operation. The effects of engine-augmenter spacing, augmenter diameter and inlet design, aft cell wall location, test cell by-pass ratio, call inlet conditions and stack-augmenter geometry on the flow field and augmenter pressure rise have been calculated. The models appear to be qualitatively correct and adequate for their intended purposes but model validation with experiment is required.
Description
Reproduction of all or part of this report is authorized.
NPS Report Number
NPS-67Nt76121Related items
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