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Analytical and Experimental Investigation of Annular Propulsive Nozzles.

Author: Ralph R Conley; Joe D Hoffman; H D Thompson; MCDONNELL DOUGLAS ELECTRONICS CO ST LOUIS MO.
Publisher: Ft. Belvoir Defense Technical Information Center MAR 1993.
Edition/Format:   eBook : English
Summary:
The final report consists of AIAA papers. The report presents an analytical performance prediction methodology for annular propulsion nozzles with and without swirl introduced in the combustor upstream of the nozzle. Four types of swirlers were investigated: free vortex, constant angle, forced vortex and Rankine vortex swirlers. For the no-swirl case thrust efficiencies and static pressure profiles from cold flow  Read more...
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Material Type: Internet resource
Document Type: Internet Resource
All Authors / Contributors: Ralph R Conley; Joe D Hoffman; H D Thompson; MCDONNELL DOUGLAS ELECTRONICS CO ST LOUIS MO.
OCLC Number: 227790499
Notes: Prepared in cooporation with Perdue University, West Lafayette, IN.
Description: 37 pages

Abstract:

The final report consists of AIAA papers. The report presents an analytical performance prediction methodology for annular propulsion nozzles with and without swirl introduced in the combustor upstream of the nozzle. Four types of swirlers were investigated: free vortex, constant angle, forced vortex and Rankine vortex swirlers. For the no-swirl case thrust efficiencies and static pressure profiles from cold flow testing of selected nozzles are summarized and compared to the predictions ... Ramjets, Supersonics.

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Primary Entity

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