Internal Aerodynamics of Turbojet Test Cells
Speakman_Internal_Aerodynamics_1976_Redacted.pdf (1.980Mb)Date
1976-12Metadata
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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.
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NPS Report Number
NPS-67Nt76121Related items
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