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Internal Aerodynamics of Turbojet Test Cells

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Author
Speakman, G. C.
Hayes, J. D.
Netzer, D. W.
Date
1976-12
Second Reader
Bell, R. W.
Metadata
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Abstract
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.
URI
http://hdl.handle.net/10945/35242
NPS Report Number
NPS-67Nt76121
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Related items

Showing items related by title, author, creator and subject.

  • Thumbnail

    An investigation of the flow in turbojet test cell augmenters. 

    Hayes, Jack Douglas (Monterey, California. Naval Postgraduate School, 1975-09);
    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 ...
  • Thumbnail

    Determination of the Momentum Drag within the Turbojet Engine Laboratory While Operating the J-57-8B Turbojet Engine 

    Naval Postgraduate School, Monterey, CA.; Aeronautics (Monterey, California. Naval Postgraduate School, 1964-09); Technical Note No. 64T-6
    Limited tests were conducted at the USNPGS Astro /Aeronautical Propulsion Laboratories to determine the magnitude and variation of the momentum drag which is developed within turboject engine test chamber while operating ...
  • Thumbnail

    Summary report of the turbojet test chamber acceptance tests conducted 11-12 December 1963 

    Hardy, H.D.; Bell, R.W. (Monterey, California. Naval Postgraduate School, 1963);
    Acceptance testing of the Turbojet Engine Test Chamber was conducted during the week of 9 December 1963 by personnel from the U.S. Naval Post­ graduate School, Department of Aeronautics, from the Overhaul and Repair ...
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