Influence of ramp location in a strut based scramjet combustor under-reacting and non-reacting flow fields

[1]  K. Pandey,et al.  Effect of transverse fuel injection system on combustion efficiency in scramjet combustor , 2021 .

[2]  Obula Reddy Kummitha,et al.  Numerical analysis of hydrogen fueled scramjet combustor with innovative designs of strut injector , 2020 .

[3]  Zhenguo Wang,et al.  Combustion modes periodical transition in a hydrogen-fueled scramjet combustor with rear-wall-expansion cavity flameholder , 2020 .

[4]  S. O’Byrne,et al.  The Effect of Fuel Injection Location on Supersonic Hydrogen Combustion in a Cavity-Based Model Scramjet Combustor , 2020, Energies.

[5]  Obula Reddy Kummitha,et al.  Numerical investigation of wavy wall strut fuel injector for hydrogen fueled scramjet combustor , 2019 .

[6]  Yingkun Li,et al.  Role of the backward-facing steps at two struts on mixing and combustion characteristics in a typical strut-based scramjet with hydrogen fuel , 2019, International Journal of Hydrogen Energy.

[7]  R. Moradi,et al.  Effect of fuel jet arrangement on the mixing rate inside trapezoidal cavity flame holder at supersonic flow , 2019, International Journal of Hydrogen Energy.

[8]  K. Jayaraman,et al.  The Effect of Transverse Injection Upstream of an Axisymmetric Aft Wall Angled Cavity in a Supersonic Flow Field , 2019, Journal of Physics: Conference Series.

[9]  K. Pandey,et al.  Numerical investigation on influence of diamond shaped strut on the performance of a scramjet combustor , 2019, International Journal of Hydrogen Energy.

[10]  Rajiv Kumar,et al.  Supersonic combustion of hydrogen using an improved strut injection scheme , 2019, International Journal of Hydrogen Energy.

[11]  Peng Zhang,et al.  Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor , 2019, Proceedings of the Combustion Institute.

[12]  K. Jayaraman,et al.  Effect of Axisymmetric Aft Wall Angle Cavity in Supersonic Flow Field , 2018 .

[13]  S Jeyakumar,et al.  Experimental study on the characteristics of axisymmetric cavity actuated supersonic flow , 2017 .

[14]  Peng Zhang,et al.  Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection , 2017 .

[15]  Obula Reddy Kummitha,et al.  Numerical analysis of scramjet combustor with innovative strut and fuel injection techniques , 2017 .

[16]  A. De,et al.  Investigation of strut-ramp injector in a Scramjet combustor: Effect of strut geometry, fuel and jet diameter on mixing characteristics , 2017, Journal of Mechanical Science and Technology.

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

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

[19]  Li Yan,et al.  Numerical investigation on the ram–scram transition mechanism in a strut-based dual-mode scramjet combustor , 2016 .

[20]  Ryan J Clark,et al.  A review of numerical simulation and modeling of combustion in scramjets , 2015 .

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

[22]  Campbell D. Carter,et al.  Experimental Studies of Pylon-Aided Fuel Injection into a Supersonic Crossflow , 2008 .

[23]  Mark Gruber,et al.  Pylon Fuel Injector Design for a Scramjet Combustor (Postprint) , 2007 .

[24]  S. Jeyakumar,et al.  Experimental Investigations on Supersonic Stream Past Axisymmetric Cavities , 2005 .

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

[26]  Franz Mayinger,et al.  Self-Ignition and Supersonic Reaction of Pylon-Injected Hydrogen Fuel , 2000 .

[27]  Goro Masuya,et al.  Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts , 1995 .

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

[29]  W. Waidmann,et al.  An experimental investigation of the combustion of a hydrogen jet injected parallel in a supersonic air stream , 1991 .