Performance Characteristics of an Annular Conical Aerospike Nozzle with Freestream Effect

Verma, SB Performance Characteristics of an Annular Conical Aerospike Nozzle with Freestream Effect. Journal of Propulsion and Power. ISSN 0748-4658

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Abstract

Anexperimental investigation has been carried out to study the performance and base pressure characteristics of a Mach 2.0 annular conical aerospike nozzle with and without freestream flow. The effect of cowl length, plug length, and plug contour variation on the nozzle performance and base pressure characteristics is studied. It is observed that the overexpansion shock from the internal nozzle, overexpansion shock on the spike surface, and the expansion fan from the cowl lip of the internal nozzle dominate the overall flowfield development. The presence of freestream flow reduces the nozzle performance by approximately 4% relative to static conditions. Base pressure characteristics are observed to be strongly influenced by the movement of these shocks on the plug surface, and their subsequent interaction with the inner shear layer controls the base-wake closure. Relative to the conical plug configuration, the contoured plug shows considerably enhanced base pressure characteristics. Real-time pressure measurements on the spike reveal highly unsteady flow in the intermittent region of separation.

Item Type: Article
Subjects: ASTRONAUTICS > Spacecraft Propulsion & Power
Depositing User: Dr. Shashi Verma
Date Deposited: 22 Aug 2014 08:11
Last Modified: 22 Aug 2014 08:11
URI: http://nal-ir.nal.res.in/id/eprint/12000

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