Numerical investigation on a typical scramjet combustor using cavity floor H2 fuel injection strategy

[1]  A. Ingenito,et al.  The investigation of inclined AFT wall cavities in a circular scramjet combustor , 2022, International Journal of Engine Research.

[2]  A. Ingenito,et al.  The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor , 2021, Energies.

[3]  S. Hosseini,et al.  Mixing efficiency of hydrogen multijet through backward-facing steps at supersonic flow , 2021 .

[4]  Wei Huang,et al.  Design exploration on the mixing augmentation induced by the oblique shock wave and a novel step in a supersonic flow , 2021 .

[5]  Li Yan,et al.  Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine , 2021 .

[6]  R. Moradi,et al.  Effect of strut angle on performance of hydrogen multi-jets inside the cavity at combustion chamber , 2020 .

[7]  R. Moradi,et al.  Computational study of the multi hydrogen jets in presence of the upstream step in a Ma=4 supersonic flow , 2020 .

[8]  R. Moradi,et al.  Computational investigation of multi hydrogen jets at inclined supersonic flow , 2020, International Journal of Energy Research.

[9]  Wei Huang,et al.  Hydrogen fuel in scramjet engines - A brief review , 2020 .

[10]  Wei Huang,et al.  Influence of the secondary flow control on the transverse gaseous injection flow field properties in a supersonic flow , 2019 .

[11]  Yingkun Li,et al.  Numerical investigation on the performance of scramjet combustor with a novel strut configuration , 2019, Applied Thermal Engineering.

[12]  Wei Huang,et al.  Recent advances in cavity-based scramjet engine- a brief review , 2019, International Journal of Hydrogen Energy.

[13]  Daren Yu,et al.  Research progress on strut-equipped supersonic combustors for scramjet application , 2018, Progress in Aerospace Sciences.

[14]  Zhenguo Wang,et al.  Ignition processes and modes excited by laser-induced plasma in a cavity-based supersonic combustor , 2018, Applied Energy.

[15]  R. Moradi,et al.  Shape effect of cavity flameholder on mixing zone of hydrogen jet at supersonic flow , 2018, International Journal of Hydrogen Energy.

[16]  Krishna Murari Pandey,et al.  Effect of variation of inlet boundary conditions on the combustion flow-field of a typical double cavity scramjet combustor , 2018 .

[17]  Gautam Choubey,et al.  Effect of different wall injection schemes on the flow-field of hydrogen fuelled strut-based scramjet combustor , 2018 .

[18]  Shibin Li,et al.  Parametric effect on the mixing of the combination of a hydrogen porthole with an air porthole in transverse gaseous injection flow fields , 2017 .

[19]  Krishna Murari Pandey,et al.  Effect of variation of hydrogen injection pressure and inlet air temperature on the flow-field of a typical double cavity scramjet combustor , 2017 .

[20]  Krishna Murari Pandey,et al.  A brief review on the recent advances in scramjet engine , 2017 .

[21]  Gautam Choubey,et al.  Effect of different strut + wall injection techniques on the performance of two-strut scramjet combustor , 2017 .

[22]  Gautam Choubey,et al.  Effect of parametric variation of strut layout and position on the performance of a typical two-strut based scramjet combustor , 2017 .

[23]  Davood Domiri Ganji,et al.  The flow feature of transverse hydrogen jet in presence of micro air jets in supersonic flow , 2017 .

[24]  Hamoon Pourmirzaagha,et al.  Characteristics of transverse hydrogen jet in presence of multi air jets within scramjet combustor , 2017 .

[25]  Wei Huang,et al.  Parametric effect on the flow and mixing properties of transverse gaseous injection flow fields with streamwise slot: A numerical study , 2017 .

[26]  Gautam Choubey,et al.  Computational Investigation of Multi-Strut Injection of Hydrogen in a Scramjet Combustor , 2017 .

[27]  Hamoon Pourmirzaagha,et al.  The influence of micro air jets on mixing augmentation of transverse hydrogen jet in supersonic flow , 2016 .

[28]  Gautam Choubey,et al.  Investigation on the effects of operating variables on the performance of two-strut scramjet combustor , 2016 .

[29]  Zhenguo Wang,et al.  Large Eddy Simulation of the flame stabilization process in a scramjet combustor with rearwall-expansion cavity , 2016 .

[30]  Ajoy Debbarma,et al.  Computational simulation of multi-strut central lobed injection of hydrogen in a scramjet combustor , 2016 .

[31]  Gautam Choubey,et al.  Effect of variation of angle of attack on the performance of two-strut scramjet combustor , 2016 .

[32]  Davood Domiri Ganji,et al.  Comparison of the single/multi transverse jets under the influence of shock wave in supersonic crossflow , 2016 .

[33]  Wei Huang Transverse jet in supersonic crossflows , 2016 .

[34]  Zhenguo Wang,et al.  Numerical simulation on ignition transients of hydrogen flame in a supersonic combustor with dual-cavity , 2016 .

[35]  Zhiwei Huang,et al.  Large eddy simulation of strut enhanced mixing for supersonic combustion , 2016 .

[36]  Gautam Choubey,et al.  Numerical Investigation on Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injector at a Flight Mach Number of 6 , 2016 .

[37]  Wei Huang Investigation on the effect of strut configurations and locations on the combustion performance of a typical scramjet combustor , 2015 .

[38]  Zhenguo Wang,et al.  Numerical and experimental study on flame structure characteristics in a supersonic combustor with dual-cavity , 2015 .

[39]  A. Fan,et al.  Flame-anchoring mechanisms of a micro cavity-combustor for premixed H2/air flame , 2015 .

[40]  Xianggeng Wei,et al.  Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor , 2015 .

[41]  M. Sun,et al.  Flame Flashback in a Supersonic Combustor Fueled by Ethylene with Cavity Flameholder , 2015 .

[42]  A. Ghoniem,et al.  The anchoring mechanism of a bluff-body stabilized laminar premixed flame , 2014 .

[43]  Antonella Ingenito,et al.  A review on hydrogen industrial aerospace applications , 2014 .

[44]  Ning Qin,et al.  Simulations of combustion with normal and angled hydrogen injection in a cavity-based supersonic combustor , 2014 .

[45]  Haiyan Wu,et al.  Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor , 2013 .

[46]  Li Yan,et al.  Progress in research on mixing techniques for transverse injection flow fields in supersonic crossflows , 2013, Journal of Zhejiang University SCIENCE A.

[47]  E. Giacomazzi,et al.  Large Eddy simulation of turbulent hydrogen-fuelled supersonic combustion in an air cross-flow , 2013 .

[48]  Lin Ma,et al.  Effect of geometric parameters on the drag of the cavity flameholder based on the variance analysis method , 2012 .

[49]  D. Mishra,et al.  Numerical Study of Effect of Fuel Injection Angle on the Performance of a 2D Supersonic Cavity Combustor , 2012 .

[50]  Wei Huang,et al.  Parametric effects on the combustion flow field of a typical strut-based scramjet combustor , 2011 .

[51]  G. Masuya,et al.  Numerical study on the turbulent structure of transverse jet into supersonic flow , 2011 .

[52]  Antonella Ingenito,et al.  Hydrogen/air supersonic combustion for future hypersonic vehicles , 2011 .

[53]  C. Bruno,et al.  The role of the baroclinic term in supersonic fuel/air mixing enhancement , 2011 .

[54]  Wei Huang,et al.  Effect of cavity flame holder configuration on combustion flow field performance of integrated hypersonic vehicle , 2010 .

[55]  Yung-Hwan Byun,et al.  A Study of the Mixing Characteristics for Cavity Sizes in SCRamjet Engine Combustor , 2009 .

[56]  S. Menon,et al.  Simulation of Turbulent Mixing Behind a Strut Injector in Supersonic Flow , 2009 .

[57]  Jianhan Liang,et al.  Flame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity Flameholder , 2008 .

[58]  Sang-Hyeon Lee,et al.  Characteristics of Dual Transverse Injection in Scramjet Combustor, Part 1: Mixing , 2006 .

[59]  Campbell D. Carter,et al.  Stability limits of cavity-stabilized flames in supersonic flow , 2005 .

[60]  Campbell D. Carter,et al.  Mixing and combustion studies using cavity-based flameholders in a supersonic flow , 2004 .

[61]  S. Baek,et al.  Numerical study on supersonic combustion with cavity-based fuel injection , 2004 .

[62]  E. T. Curran,et al.  Scramjet Engines: The First Forty Years , 2001 .

[63]  Ronald K. Hanson,et al.  Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview , 2001 .

[64]  Michael Oevermann,et al.  Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling , 2000 .

[65]  K. Hsu,et al.  Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors , 1999 .

[66]  M. Gruber,et al.  A study of recessed cavity flowfields for supersonic combustion applications , 1998 .

[67]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[68]  F. Billig Research on supersonic combustion , 1992 .

[69]  J. Schetz,et al.  Analysis of slot injection in hypersonic flow , 1991 .

[70]  F. S. Billig,et al.  The interaction and penetration of gaseous jets in supersonic flow , 1969 .