Impact of axial vortices on mixing at a high convective Mach number

Bernard Parent; Jean P. Sislian

doi:10.2514/2.2086

Impact of axial vortices on mixing at a high convective Mach number

Bernard Parent, Jean P. Sislian

Research output: Contribution to journal › Article › peer-review

9 Scopus citations

Abstract

The increase in mixing induced by the axial vortices of the cantilevered ramp injector at a high convective Mach number of 1.5 was assessed. The problems investigated are representative of inert mixing occurring in a shcramjet inlet. Results were obtained with the Window Allocatable Resolver for Propulsion (WARP).

Original language	English (US)
Pages (from-to)	1386-1388
Number of pages	3
Journal	AIAA journal
Volume	41
Issue number	7
DOIs	https://doi.org/10.2514/2.2086
State	Published - Jul 2003
Externally published	Yes

ASJC Scopus subject areas

Aerospace Engineering

Access to Document

10.2514/2.2086

Cite this

@article{75f97340a3484eebbd5d00a537ada90a,

title = "Impact of axial vortices on mixing at a high convective Mach number",

abstract = "The increase in mixing induced by the axial vortices of the cantilevered ramp injector at a high convective Mach number of 1.5 was assessed. The problems investigated are representative of inert mixing occurring in a shcramjet inlet. Results were obtained with the Window Allocatable Resolver for Propulsion (WARP).",

author = "Bernard Parent and Sislian, {Jean P.}",

year = "2003",

month = jul,

doi = "10.2514/2.2086",

language = "English (US)",

volume = "41",

pages = "1386--1388",

journal = "AIAA journal",

issn = "0001-1452",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "7",

}

TY - JOUR

T1 - Impact of axial vortices on mixing at a high convective Mach number

AU - Parent, Bernard

AU - Sislian, Jean P.

PY - 2003/7

Y1 - 2003/7

N2 - The increase in mixing induced by the axial vortices of the cantilevered ramp injector at a high convective Mach number of 1.5 was assessed. The problems investigated are representative of inert mixing occurring in a shcramjet inlet. Results were obtained with the Window Allocatable Resolver for Propulsion (WARP).

AB - The increase in mixing induced by the axial vortices of the cantilevered ramp injector at a high convective Mach number of 1.5 was assessed. The problems investigated are representative of inert mixing occurring in a shcramjet inlet. Results were obtained with the Window Allocatable Resolver for Propulsion (WARP).

UR - http://www.scopus.com/inward/record.url?scp=0041311107&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0041311107&partnerID=8YFLogxK

U2 - 10.2514/2.2086

DO - 10.2514/2.2086

M3 - Article

AN - SCOPUS:0041311107

SN - 0001-1452

VL - 41

SP - 1386

EP - 1388

JO - AIAA journal

JF - AIAA journal

IS - 7

ER -

Impact of axial vortices on mixing at a high convective Mach number

Abstract

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this