Abstract
Hypersonic aircraft are flight vehicles which operate at a Mach number higher than 5, including hypersonic cruise aircraft, hypersonic cruise missiles, and reusable orbital aerospace planes. Since these hypersonic vehicles have revolutionary applications in commercial aviation, national security, and space exploration, great effort has been dedicated to their development since the 1950s (Curran in J Propul Power 17:1138–1148, 2001).
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Almeida H, Sousa JMM, Costa M (2014) Effect of the liquid injection angle on the atomization of liquid jets in subsonic crossflows. At Sprays 24:81–96. https://doi.org/10.1615/AtomizSpr.2013008310
Becker J, Hassa C (2002) Breakup and atomization of a kerosene jet in crossflow at elevated pressure. At Sprays 12:49–68. https://doi.org/10.1615/AtomizSpr.v12.i123.30
Ben-Yakar A, Hanson R (1999) Hypervelocity combustion studies using simultaneous OH-PLIF and Schlieren imaging in an expansion tube. In: 35th joint propulsion conference and exhibit. American Institute of Aeronautics and Astronautics, Reston, Virginia, p 47
Ben-Yakar A, Mungal MG, Hanson RK (2006) Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows. Phys Fluids 18:26101. https://doi.org/10.1063/1.2139684
Billig FS, Schetz JA (1966) Penetration of gaseous jets injected into a supersonic stream. J Spacecr Rockets 3:1658–1665. https://doi.org/10.2514/3.28721
Chai X, Iyer PS, Mahesh K (2015) Numerical study of high speed jets in crossflow. J Fluid Mech 785:152–188. https://doi.org/10.1017/jfm.2015.612
Chai X, Mahesh K (2011) Simulations of high speed turbulent jets in crossflows. In: 49th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition 2011
Constantine PG, Emory M, Larsson J, Iaccarino G (2015) Exploiting active subspaces to quantify uncertainty in the numerical simulation of the HyShot II scramjet. J Comput Phys 302:1–20
Curran ET (2001) Scramjet engines: the first forty years. J Propul Power 17:1138–1148. https://doi.org/10.2514/2.5875
Cutler AD, Harding GC, Diskin GS (2013) High frequency pulsed injection into a supersonic duct flow. AIAA J 51:809–818. https://doi.org/10.2514/1.J051620
Deneys R, Diwakar R (1987) Structure of high-pressure fuel sprays. SAE Paper 870598
Dickmann DA, Lu FK (2009) Shock/boundary-layer interaction effects on transverse jets in crossflow over a flat plate. J Spacecr Rockets 46:1132–1141. https://doi.org/10.2514/1.39297
Dziuba M, Rossmann T (2006) Super sonic mixing enhancement by means of high powered jet modulation. In: 44th AIAA aerospace sciences meeting and exhibit
Elshamy OM, Tambe SB, Cai J, Jeng SM (2007) PIV and LDV measurements for liquid jets in crossflow. Paper presented at the AIAA 2007-1338, Nevada
Erdem E, Saravanan S, Lin J, Kontis K (2012) Experimental investigation of transverse injection flowfield at March 5 and the influence of impinging shock wave. In: 18th AIAA/3AF international space planes, p 205
Fei LS, Xu SL, Wang CJ, Qiang L, Huang SH (2008) Experimental study on atomization phenomena of kerosene in supersonic cold flow. Sci China 51(2):145–152
Fric TF, Roshko A (1994) Vortical structure in the wake of a transverse jet. J Fluid Mech 279:1. https://doi.org/10.1017/S0022112094003800
Gamba M, Mungal MG (2015) Ignition, flame structure and near-wall burning in transverse hydrogen jets in supersonic crossflow. J Fluid Mech 780:226–273. https://doi.org/10.1017/jfm.2015.454
Génin F, Menon S (2010) Dynamics of sonic jet injection into supersonic crossflow. J Turbul 11:N4. https://doi.org/10.1080/14685240903217813
Gruber MR, Nejad AS, Chen TH, Dutton JC (1997) Compressibility effects in supersonic transverse injection flowfields. Phys Fluids 9:1448–1461. https://doi.org/10.1063/1.869257
Gruber MR, Nejad AS, Chen TH, Dutton JC (2000) Transverse injection from circular and elliptic nozzles into a supersonic crossflow. J Propul Power 16:449–457. https://doi.org/10.2514/2.5609
Huang W, J-g Tan, Liu J, Yan L (2015) Mixing augmentation induced by the interaction between the oblique shock wave and a sonic hydrogen jet in supersonic flows. Acta Astronaut 117:142–152. https://doi.org/10.1016/j.actaastro.2015.08.004
Huang W, Wang Z-g Wu, J-p Li S-b (2013) Numerical prediction on the interaction between the incident shock wave and the transverse slot injection in supersonic flows. Aerosp Sci Technol 28:91–99. https://doi.org/10.1016/j.ast.2012.10.007
Im K-S, Lin K-C, Lai M-C, Chon MS (2011) Breakup modeling of a liquid jet in cross flow. Int J Automot Technol 12:489–496. https://doi.org/10.1007/s12239-011-0057-1
Kawai S, Lele SK (2010) Large-eddy simulation of jet mixing in supersonic crossflows. AIAA J 48:2063–2083. https://doi.org/10.2514/1.J050282
Kim C-H, Jeung I-S, Choi B, Kouchi T, Masuya G (2012) Flowfield characteristics of a hypermixer interacting with transverse injection in supersonic flow. AIAA J 50:1742–1753. https://doi.org/10.2514/1.J051588
Kim JS, Kim JS (2009) A characterization of the spray evolution by dual-mode phase doppler anemometry in an injector of liquid-propellant thruster. J Mech Sci Technol 23(6):1637–1649.
Koh H, Jung K, Yoon Y, Lee K, Jeong KS (2006) Development of quantitative measurement of fuel mass distribution using planar imaging technique. J Vis 9(2):161–170
Kolpin MA, Horn KP, Reichenbach RE (1968) Study of penetration of a liquid injectant into a supersonic flow. AIAA J 6(5):853–858
Kouchi T, Sasaya K, Watanabe J, Shibayama H, Masuya G (2010) Penetration characteristics of pulsed injection into supersonic crossflow. In: 46th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit. American Institute of Aeronautics and Astronautics, Reston, VA, p 697
Kourmatzis A, Masri AR (2014) The influence of gas phase velocity fluctuations on primary atomization and droplet deformation. Exp Fluids 55:245. https://doi.org/10.1007/s00348-013-1659-3
Larsson J, Laurence S, Bermejo-Moreno I, Bodart J, Karl S, Vicquelin R (2015) Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part II: Large eddy simulations. Combust Flame 162(4):907–920
Lee I, Kang Y, Koo J (2010a) Mixing characteristics of pulsed air-assist liquid jet into an internal subsonic crossflow. J Therm Sci 19(2):136–140
Lee IC, Kang YS, Moon HJ, Jang SP, Kim JK, Koo J (2010b) Spray jet penetration and distribution of modulated liquid jets in subsonic crossflows. J Mech Sci Technol 24(7):1425–1431. https://doi.org/10.1007/s12206-010-0418-0
Lee J, Sallam KA, Kin KC (2015) Spray structure in near-injector region of aerated jet in subsonic crossflow. J Propuls Power 25(2):11
Lee S-H (2006) Characteristics of dual transverse injection in scramjet combustor, Part 1: Mixing. J Propul Power 22:1012–1019. https://doi.org/10.2514/1.14180
Lin KC, Kennedy PJ, Jackson TA (2000) Spray penetration heights of angled-injected aerated-liquid jets in supersonic crossflows. In: 38th aerospace sciences meeting & exhibit, 1–13
Lin KC, Kennedy P, Jackson T (2004) Structures of water jets in a Mach 1.94 supersonic crossflow. In: AIAA Aerospace sciences meeting and exhibit, 2004
Lin K-C, Kennedy P, Jackson T (2002) Penetration heights of liquid jets in high-speed crossflows. In: 40th AIAA aerospace sciences meeting & exhibit. American Institute of Aeronautics and Astronautics, Reston, VA, p 2002
Liu AB, Mather D, Reitz RD (1993) Modeling the effects of drop drag and breakup on fuel sprays. Sae Paper 93
Mashayek A, Behzad M, Ashgriz N (2011) Multiple injector model for primary breakup of a liquid jet in crossflow. AIAA J 49:2407–2420. https://doi.org/10.2514/1.J050623
Mcdaniel JC, Raves J (1988) Laser-induced-fluorescence visualization of transverse gaseous injection in a nonreacting supersonic combustor. J Propul Power 4:591–597. https://doi.org/10.2514/3.23105
Micka DJ, Driscoll JF (2012) Stratified jet flames in a heated (1390 K) air cross-flow with autoignition. Combust Flame 159:1205–1214. https://doi.org/10.1016/j.combustflame.2011.10.013
Moraitis C, Riethmuller M (1988) Particle image displacement velocimetry applied in high speed flows. Paper presented at the 4th international symposium on applications of laser anemometry to fluid dynamic
Murugappan S, Gutmark E, Carter C (2005) Control of penetration and mixing of an excited supersonic jet into a supersonic cross stream. Phys Fluids 17:106101. https://doi.org/10.1063/1.2099027
Nakaya S, Hikichi Y, Nakazawa Y, Sakaki K, Choi M, Tsue M, Kono M, Tomioka S (2015) Ignition and supersonic combustion behavior of liquid ethanol in a scramjet model combustor with cavity flame holder. Proc Combust Inst 35(2):2091–2099
Olinger DS, Sallam KA, Lin K-C (2014) Digital holographic analysis of the near field of aerated-liquid jets in crossflow. J Propul Power 30(6):1636–1645
O’Rourke PJ, Amsden AA (1987) The tab method for numerical calculation of spray droplet breakup. In: SAE Technical Paper Series. SAE international 400 commonwealth drive, Warrendale, PA, United States
Patterson MA, Reitz RD (1998) Modeling the effects of fuel spray characteristics on diesel engine combustion and emission. In: SAE Technical Paper Series. SAE international 400 commonwealth drive, Warrendale, PA, United States
Portz R, Segal C (2006) Penetration of gaseous jets in supersonic flows. AIAA J 44:2426–2429. https://doi.org/10.2514/1.23541
Rachner M, Becker J, Hassa C (2002) Modelling of the atomization of a plain liquid fuel jet in crossflow at gas turbine conditions. Aerosp Sci Technol 6(7):495–506
Randolph H, Chew L, Johari H (1994) Pulsed jets in supersonic crossflow. J Propul Power 10:746–748. https://doi.org/10.2514/3.23790
Rothstein A, Wantuck P (1992) A study of the normal injection of hydrogen into a heated supersonicflow using planar laser-induced fluorescence. In: 28th joint propulsion conference 1992, p 591
Shan JW, Dimotakis PE (2006) Reynolds-number effects and anisotropy in transverse-jet mixing. J Fluid Mech 566:47–96
Schetz JA, Maddalena L, Burger SK (2010) Molecular weight and shock-wave effects on transverse injection in supersonic flow. J Propul Power 26:1102–1113. https://doi.org/10.2514/1.49355
Sun M-B, Zhang S, Zhao Y, Zhao Y, Liang J (2013) Experimental investigation on transverse jet penetration into a supersonic turbulent crossflow. Sci China Technol Sci 56:1989–1998. https://doi.org/10.1007/s11431-013-5265-7
Tahsini AM, Mousavi ST (2015) Investigating the supersonic combustion efficiency for the jet-in-cross-flow. Int J Hydrog Energ 40:3091–3097. https://doi.org/10.1016/j.ijhydene.2014.12.124
Takahashi H, Ikegami S, Masuya G, Hirota M (2010) Extended quantitative fluorescence imaging for multicomponent and staged injection into supersonic crossflows. J Propul Power 26:798–807. https://doi.org/10.2514/1.47318
Urzay J (2018) Supersonic combustion in air-breathing propulsion systems for hypersonic flight. Annu Rev Fluid Mech 50:593–627. https://doi.org/10.1146/annurev-fluid-122316-045217
VanLerberghe WM, Santiago JG, Dutton JC, Lucht RP (2000) Mixing of a sonic transverse jet injected into a supersonic flow. AIAA J 38:470–479. https://doi.org/10.2514/2.984
Vinogradov VA, Shikhman YM, Segal C (2007) A review of fuel pre-injection in supersonic, chemically reacting flows. Appl Mech Rev 60(4). https://doi.org/10.1115/1.2750346
Viti V, Neel R, Schetz JA (2009) Detailed flow physics of the supersonic jet interaction flow field. Phys Fluids 21:46101. https://doi.org/10.1063/1.3112736
Wang D-P, Zhao Y, Xia Z-X, Wang Q-H, Huang L (2012a) Experimental investigation of supersonic flow over a hemisphere. Chin Sci Bull 57:1765–1771. https://doi.org/10.1007/s11434-012-5124-0
Wang D-P, Zhao Y-X, Xia Z-X, Wang Q-H, Luo Z-B (2012b) Flow visualization of supersonic flow over a finite cylinder. Chin Phys Lett 29:84702. https://doi.org/10.1088/0256-307X/29/8/084702
Wang G-L, Chen L, Lu X-Y (2013) Effects of the injector geometry on a sonic jet into a supersonic crossflow. Sci China Phys Mech Astron 56:366–377. https://doi.org/10.1007/s11433-012-4984-2
Westerweel J, Elsinga GE, Adrian RJ (2013) Particle image velocimetry for complex and turbulent flows. Annu Rev Fluid Mech 45(1):409–436
Williams NJ (2016) Numerical investigations of a high frequency pulsed gaseous fuel jet injection into a supersonic crossflow. Doctoral dissertation, University of Tennessee
Wu PK, Kirkendall KA (1998) Spray structures of liquid jets atomized in subsonic cross-flows. J Propul Power 14(2):10–17
Xiao F, Wang ZG, Sun MB, Liang JH, Liu N (2016) Large eddy simulation of liquid jet primary breakup in supersonic air crossflow. Int J Multiph Flow 87:229–240
Xie J, Gan ZW, Duan F, Wong TN, Yu MC, Zhao R (2013) Characterization of spray atomization and heat transfer of pressure swirl nozzles. Int J Therm Sci 68:94–102
Yang H, Li F, Sun B (2012) Trajectory Analysis of Fuel injection into supersonic cross flow based on Schlieren method. Chin J Aeronaut 25:42–50. https://doi.org/10.1016/S1000-9361(11)60360-9
Yang H, Li F, Sun B (2012) Trajectory analysis of fuel injection into supersonic cross flow based on Schlieren method. Chin J Aeronaut 25:42–50. https://doi.org/10.1016/S1000-9361(11)60360-9
Yoon HJ, Hong JG, Lee C-W (2011) Correlations for penetration height of single and double liquid jets in cross flow under high-temperature conditions. Atomiz Spr 21:673–686. https://doi.org/10.1615/AtomizSpr.2012004212
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2019 Springer Nature Singapore Pte Ltd.
About this chapter
Cite this chapter
Sun, M., Wang, H., Xiao, F. (2019). Introduction. In: Jet in Supersonic Crossflow. Springer, Singapore. https://doi.org/10.1007/978-981-13-6025-1_1
Download citation
DOI: https://doi.org/10.1007/978-981-13-6025-1_1
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-13-6024-4
Online ISBN: 978-981-13-6025-1
eBook Packages: EngineeringEngineering (R0)