44th AIAA Aerospace Sciences Meeting and Exhibit 2006
DOI: 10.2514/6.2006-1229
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Penetration of Gaseous Jets In Supersonic Flows

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Cited by 11 publications
(26 citation statements)
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“…To satisfy the requirements in engineering, researchers mainly focus on time-averaged penetration height, mass fraction distribution, total pressure loss in the following four aspects, namely jet-to-freestream momentum flux ratio [4,[14][15][16][17], injection angle [4,[18][19][20], configuration of injection orifice [4,21], molecular weight [21][22][23]. However, limited by experimental measurements and numerical simulations, the turbulent characteristics of sonic jet in supersonic crossflow are not the major contents in the early studies.…”
Section: Introductionmentioning
confidence: 98%
“…To satisfy the requirements in engineering, researchers mainly focus on time-averaged penetration height, mass fraction distribution, total pressure loss in the following four aspects, namely jet-to-freestream momentum flux ratio [4,[14][15][16][17], injection angle [4,[18][19][20], configuration of injection orifice [4,21], molecular weight [21][22][23]. However, limited by experimental measurements and numerical simulations, the turbulent characteristics of sonic jet in supersonic crossflow are not the major contents in the early studies.…”
Section: Introductionmentioning
confidence: 98%
“…And the influence of jet-to-freestream momentum flux ratio [12][13][14][15][16], configuration of injection orifice [15,17], molecular weight [17][18][19] on the averaged parameters are widely investigated for several years.…”
Section: Introductionmentioning
confidence: 99%
“…The time-averaged results obtained by hybrid RANSand computational studies[12][13][14][15][16], it is observed that penetration height of transverse jet primarily depends on jet-to-freestream momentum flux ratio J , as shown in eq.…”
mentioning
confidence: 95%
“…The jet penetration is primarily determined by the momentum flux 2 u  of fuel jet. 20,21 Assuming the cross jet is a quasi-1D process, we can write the variation of …”
Section: E Maximum Jet Momentum Fluxmentioning
confidence: 99%
“…(20), (18), (9), (10), (11) and (12) can be reduced to the classical form of differential relations of perfect gas dynamics. 19 2.…”
Section: Second Order Derivative Related Formulaementioning
confidence: 99%