nach oben

Acta Mechanica Sinica

Erschienen in:

09.09.2019 | Review

Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms

verfasst von: Wei Yao

Erschienen in: Acta Mechanica Sinica | Ausgabe 6/2019

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

A brief review of the recent advances in kerosene-fueled supersonic combustion modeling is present by comparing the fuels, reviewing the kinetic mechanisms, and introducing recent modeling results. The advantages and disadvantages of hydrogen and kerosene for the scramjet combustor are compared to show that kerosene is a more viable fuel option for a Mach number range of 4–8. However, detailed kinetic mechanisms for kerosene, which usually contain thousands of elementary reactions, must be significantly reduced for use in modeling. As of this writing, the smallest skeletal kerosene mechanism has only 19 species and 53 reversible reactions. In contrast to pioneer models based on global chemistry, the current kerosene-fueled supersonic combustion models based on reduced/skeletal chemistry are classified as second-stage. The influence of kinetic mechanisms, global equivalence ratios, inlet Mach number, geometric shape, and domain symmetry are reviewed based on high-fidelity models and available measurements. With the advances in computational technology, models with accurate descriptions of both flow and chemistry are becoming a promising, indispensable approach for the study of supersonic combustion.

Vorheriger Artikel A note on the Galilean invariance of aerodynamic force theories in unsteady incompressible flows

Nächster Artikel Experimental and numerical investigation of the influence of roughness and turbulence on LUT airfoil performance

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Curran, E.T., Murthy, S.N.B.: High-Speed Flight Propulsion Systems. American Institute of Aeronautics and Astronautics, Washington, DC (1991)

Maurice, L., Edward, T., Griffiths, J.: Liquid hydrocarbon fuels for hypersonic propulsion. Scramjet propulsion 189, 757–822 (2001)

Hui, X., Sung, C.J.: Laminar flame speeds of transportation-relevant hydrocarbons and jet fuels at elevated temperatures and pressures. Fuel 109, 191–200 (2013)

Dagaut, P., Cathonnet, M.: The ignition, oxidation, and combustion of kerosene: a review of experimental and kinetic modeling. Prog. Energy Combust. Sci. 32, 48–92 (2006)

Vasu, S.S., Davidson, D.F., Hanson, R.K.: Jet fuel ignition delay times: shock tube experiments over wide conditions and surrogate model predictions. Combust. Flame 152, 125–143 (2008)

Fiorina, B., Vié, A., Franzelli, B., et al.: Modeling challenges in computing aeronautical combustion chamber. Aerospacelab J. 11, 1–19 (2016)

Yan, Y., Liu, Y., Di, D., et al.: Simplified chemical reaction mechanism for surrogate fuel of aviation kerosene and its verification. Energy Fuels 30, 10847–10857 (2016)

Kundu, K.P., Deur, J.M.: A simplified reaction mechanism for calculation of emissions in hydrocarbon (jet-a) combustion. In: AIAA/SAE/ASME/ASEE 29th joint propulsion conference and exhibit. Monterey, CA, 28–30 June (1993)

Gueret, C., Cathonnet, M., Boettner, J.C., et al.: Experimental study and modeling of kerosene oxidation in a jet-stirred flow reactor. Symposium (International) on Combustion 23, 211–216 (1991)

10.

Schulz, W.D.: Oxidation products of a surrogate JP-8 fuel. ACS Petrol. Chem. Div. Preprints 37, 383–392 (1991)

11.

Heneghan, S.P., Locklear, S.L., Geiger, D.L.I., et al.: Static tests of jet fuel thermal and oxidative stability. J. Propul. Power 9, 5–9 (1993)

12.

Violi, A., Yan, S., Eddings, E.G., et al.: Experimental formulation and kinetic model for JP-8 surrogate mixtures. Combust. Sci. Technol. 174, 399–417 (2002)

13.

Cooke, J.A., Bellucci, M., Smooke, M.D., et al.: Computational and experimental study of JP-8, a surrogate, and its components in counterflow diffusion flames. Proc. Combust. Inst. 30, 439–446 (2005)

14.

Agosta, A.: Development of a chemical surrogate for JP-8 aviation fuel using a pressurized flow reactor. [Master Thesis], Drexel University (2002)

15.

Humer, S., Frassoldati, A., Granata, S., et al.: Experimental and kinetic modeling study of combustion of JP-8, its surrogates and reference components in laminar nonpremixed flows. Proc. Combust. Inst. 31, 393–400 (2007)

16.

Daniau, E., Bouchez, M., Bounaceur, R., et al.: Contribution to scramjet active cooling analysis using n-dodecane decomposition model as a generic endothermic fuel. In: 12th AIAA international space planes and hypersonic systems and technologies. Norfolk, Virginia, 15–19 December (2003)

17.

Dagaut, P., El Bakali, A., Ristori, A.: The combustion of kerosene: experimental results and kinetic modelling using 1- to 3-component surrogate model fuels. Fuel 85, 944–956 (2006)

18.

Colket, M., Edwards, T., Williams, S., et al.: Development of an experimental database and kinetic models for surrogate jet fuels. In: 45th AIAA aerospace sciences meeting and exhibit. Reno, Nevada, 8–11 January (2007)

19.

Honnet, S., Seshadri, K., Niemann, U., et al.: A surrogate fuel for kerosene. Proc. Combust. Inst. 32, 485–492 (2009)

20.

Lindstedt, R.P., Maurice, L.Q.: Detailed chemical-kinetic model for aviation fuels. J. Propul. Power 16, 187–195 (2000)

21.

Dooley, S., Won, S.H., Chaos, M., et al.: A jet fuel surrogate formulated by real fuel properties. Combust. Flame 157, 2333–2339 (2010)

22.

Dooley, S., Won, S.H., Heyne, J., et al.: The experimental evaluation of a methodology for surrogate fuel formulation to emulate gas phase combustion kinetic phenomena. Combust. Flame 159, 1444–1466 (2012)

23.

Moss, J.B., Aksit, I.M.: Modelling soot formation in a laminar diffusion flame burning a surrogate kerosene fuel. Proc. Combust. Inst. 31, 3139–3146 (2007)

24.

Naik, C.V., Puduppakkam, K.V., Modak, A., et al.: Detailed chemical kinetic mechanism for surrogates of alternative jet fuels. Combust. Flame 158, 434–445 (2011)

25.

Mzé-Ahmed, A., Dagaut, P., Hadj-Ali, K., et al.: Oxidation of a coal-to-liquid synthetic jet fuel: experimental and chemical kinetic modeling study. Energy Fuels 26, 6070–6079 (2012)

26.

Dagaut, P., Karsenty, F., Dayma, G., et al.: Experimental and detailed kinetic model for the oxidation of a gas to liquid (gtl) jet fuel. Combust. Flame 161, 835–847 (2014)

27.

Dagaut, P., Dayma, G., Karsenty, F., et al.: The combustion of synthetic jet fuels (gas to liquid and coal to liquid) and multi-component surrogates: Experimental and modeling study. In: Proceedings of ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Montréal, Canada, 15–19 June (2015)

28.

Fan, X., Yu, G.: Analysis of thermophysical properties of Daqing RP-3 aviation kerosene. J. Propul. Technol. 27, 187–192 (2006)

29.

Zheng, D., Yu, W., Zhong, B.: RP-3 aviation kerosene surrogate fuel and the chemical reaction kinetic model. Acta Phys. Chim. Sin. 31, 636–642 (2015)

30.

Dagaut, P., Reuillon, M., Boettner, J.C., et al.: Kerosene combustion at pressures up to 40 atm: Experimental study and detailed chemical kinetic modeling. Symposium (International) on Combustion 25, 919–926 (1994)

31.

Dagaut, P.: On the kinetics of hydrocarbons oxidation from natural gas to kerosene and diesel fuel. Phys. Chem. Chem. Phys. 4, 2079–2094 (2002)

32.

Lu, T., Law, C.K.: Toward accommodating realistic fuel chemistry in large-scale computations. Prog. Energy Combust. Sci. 35, 192–215 (2009)

33.

Hautman, D.J., Dryer, F.L., Schug, K.P., et al.: A multiple-step overall kinetic mechanism for the oxidation of hydrocarbons. Combust. Sci. Technol. 25, 219–235 (1981)

34.

Najjar, Y.S.H., Goodger, E.M.: Soot oxidation in gas turbines using heavy fuels. 2. Fuel. 60, 987–990 (1981)

35.

Najjar, Y.S.H., Goodger, E.M.: Soot formation in gas turbines using heavy fuels. 1. Fuel. 60, 980–986 (1981)

36.

Westbrook, C.K., Dryer, F.L.: Chemical kinetic modeling of hydrocarbon combustion. Prog. Energy Combust. Sci. 10, 1–57 (1984)

37.

Aly, S.L., Salem, H.: Prediction of premixed laminar flame characteristics of commercial kerosene fuel. Fuel 68, 1203–1209 (1989)

38.

Gueret, C., Cathonnet, M., Boettner, J.C., et al.: Experimental study and modeling of kerosene oxidation in a jet-stirred flow reactor. Symposium (International) on Combustion 23, 211–216 (1990)

39.

Wang, T.S.: Thermophysics characterization of kerosene combustion. J. Thermophys. Heat Transfer 15, 140–147 (2001)

40.

Franzelli, B., Riber, E., Sanjosé, M., et al.: A two-step chemical scheme for kerosene–air premixed flames. Combust. Flame 157, 1364–1373 (2010)

41.

Choi, J.Y.: A quasi global mechanism of kerosene combustion for propulsion applications. In: 47th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit. San Diego, California, 31 July–3 August (2011)

42.

Hou, L.Y., Niu, D.S., Pan, P.F., et al.: Effects of kerosene global reaction mechanisms on supersonic combustion. J. Propul. Technol. 34, 938–943 (2013)

43.

Yao, W., Wu, K., Fan, X.: Development of skeletal kerosene mechanisms and application to supersonic combustion. Energy Fuels 32, 12992–13003 (2018)

44.

Yao, W., Wang, J., Lu, Y., et al.: Skeletal mechanism generation based on DRGEPSA for Daqing RP-3 aviation kerosene and numerical validation. In: the 7th Chinese National Conference on Hypersonic Science and Technology, Beijing, 29–31 October (2014)

45.

Yao, W., Yuan, Y., Li, X., et al.: Comparative study of elliptic and round scramjet combustors fueled by RP-3. J. Propul. Power 34, 772–786 (2018)

46.

Yao, W., Lu, Y., Wu, K., et al.: Modeling analysis of an actively-cooled scramjet combustor under different kerosene/air ratios. J. Propul. Power 34, 975–991 (2018)

47.

Yao, W., Yuan, Y., Li, X., et al.: A comparative study of elliptic and round scramjet combustors by improved delayed detached eddy simulation. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China, 6–9 March (2017)

48.

Yao, W., Lu, Y., Li, X., et al.: Improved delayed detached eddy simulation of a high-ma active-cooled scramjet combustor based on skeletal kerosene mechanism. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference. Salt Lake City, Utah, 25–27 July (2016)

49.

Yao, W., Wang, J., Lu, Y., et al.: Full-scale detached eddy simulation of kerosene fueled scramjet combustor based on skeletal mechanism. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Glasgow, Scotland, 6–9 July (2015)

50.

Liu, B., He, G.Q., Qin, F., et al.: Simulation of kerosene fueled RBCC engine based on skeletal mechanism. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6–9 March (2017)

51.

Liu, Y., Liu, Y., Chen, D., et al.: A simplified mechanistic model of three-component surrogate fuels for RP-3 aviation kerosene. Energy Fuels 32, 9949–9960 (2018)

52.

Zeng, W., Liang, S., Li, H.-X., et al.: Chemical kinetic simulation of kerosene combustion in an individual flame tube. J. Adv. Res. 5, 357–366 (2014)

53.

Zeng, W., Liu, J.C., Chen, X.X., et al.: A new reduced reaction mechanism of a surrogate fuel for kerosene. Can. J. Chem. Eng. 91, 483–489 (2013)

54.

Huang, W., Chen, F., Liu, H., et al.: Modeling chemical mechanism for surrogate jet fuel under scramjet operating conditions. In: 54th AIAA Aerospace Sciences Meeting. San Diego, California, 4–8 January (2016)

55.

Xu, J., Guo, J., Liu, A., et al.: Construction of autoignition mechanisms for the combustion of RP-3 surrogate fuel and kinetics simulation. Acta Phys. Chim. Sin. 31, 643–652 (2015)

56.

Zettervall, N., Fureby, C., Nilsson, E.J.K.: A small skeletal kinetic mechanism for kerosene combustion. Energy Fuels 30, 9801–9813 (2016)

57.

Strelkova, M.I., Kirillov, I.A., Potapkin, B.V., et al.: Detailed and reduced mechanisms of jet-a combustion at high temperatures. Combust. Sci. Technol. 180, 1788–1802 (2008)

58.

Slavinskaya, N.A.: Skeletal mechanism for kerosene combustion with pah production. In: 46th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, 7–10 January (2008)

59.

Koniavitis, P., Rigopoulos, S., Jones, W.P.: Reduction of a detailed chemical mechanism for a kerosene surrogate via RCCE-CSP. Combust. Flame 194, 85–106 (2018)

60.

Yao, W., Wu, K., Lee, Y., et al.: Influence of chemical mechanisms on supersonic combustion characteristics fueled by kerosene. In: 2018 Joint Propulsion Conference, AIAA Propulsion and Energy Forum and Exposition. Cincinnati, Ohio, 9–11 July (2018)

61.

Davidson, D.F., Shao, J., Parise, T., et al.: Shock tube measurements of jet and rocket fuel ignition delay times. In: 55th AIAA Aerospace Sciences Meeting. Grapevine, Texas, 9–13 January (2017)

62.

Niemeyer, K.E., Sung, C.J., Raju, M.P.: Skeletal mechanism generation for surrogate fuels using directed relation graph with error propagation and sensitivity analysis. Combust. Flame 157, 1760–1770 (2010)

63.

Wu, K., Yao, W., Fan, X.: Development and fidelity evaluation of a skeletal ethylene mechanism under scramjet-relevant conditions. Energy Fuels 31, 14296–14305 (2017)

64.

Yao, W., Wu, K., Fan, X.: Influences of domain symmetry on supersonic combustion modeling. J. Propul. Power 35, 451–465 (2019)

65.

Wang, Y., Yao, W., Fan, X.: Real-gas effect accounted for by the principle of extended corresponding states in modeling supersonic kerosene jet. In: 2018 Joint Propulsion Conference, AIAA Propulsion and Energy Forum and Exposition. Cincinnati, Ohio, 9–11 July (2018)

66.

Li, B., Lee, Y., Yao, W., et al.: Prediction of kerosene properties at supercritical pressures by artificial neural network. In: 2018 Joint Propulsion Conference, AIAA Propulsion and Energy Forum and Exposition. Cincinnati, Ohio, 9–11 July (2018)

67.

Yao, W., Fan, X.: Development of zone flamelet model for scramjet combustor modeling. In: 21st AIAA International Space Planes and Hypersonic Systems and Technology Conference. Xiamen, China, 6–9 March (2017)

68.

Yao, W., Wang, J., Fan, E., et al.: IDDES study of the flow and combustion characteristics in a RP-3 fueled round-to-elliptical shape-transition supersonic combustor. In: the 9th Chinese National Conference on Hypersonic Science and Technology, Xi’an, 18–21 October (2016)

69.

Yao, W., Li, X., Wu, K., et al.: Detached eddy simulation of an axisymmetric scramjet combustor fueled by Daqing RP-3 aviation kerosene. In: the 8th Chinese National Conference on Hypersonic Science and Technology, Haerbing, 25–27 November (2015)

70.

Yao, W., Zheng, L., Zhang, H.: Modeling analysis on the silica glass synthesis in a hydrogen diffusion flame. Int. J. Heat Mass Transf. 81, 797–803 (2015)

71.

Fureby, C., Chapuis, M., Fedina, E., et al.: CFD analysis of the HyShot II scramjet combustor. Proc. Combust. Inst. 33, 2399–2405 (2011)

72.

Larsson, J., Vicquelin, R., Bermejo-Moreno, I.: Large eddy simulations of the hyshot II scramjet. Annual research briefs 2011, Stanford University (2011)

73.

Cecere, D., Ingenito, A., Bruno, C., et al.: Advances in LES of the hyshot II scramjet combustor. In: Processes and Technologies for a Sustainable Energy, Ischia, June 27–30 (2010)

74.

Antonella, I., Claudio, B., Donato, C.: LES of the hyshot scramjet combustor. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 4–7 January (2010)

75.

Johan, L.: Large eddy simulation of the hyshot II scramjet combustor using a supersonic flamelet model. In: 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Atlanta, Georgia, 30 July–1 August (2012)

76.

Romagnosi, L., Ingenito, A., Cecere, D., et al.: The role of the baroclinic term in supersonic fuel/air mixing enhancement. In: 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 4–7 January (2011)

77.

Cecere, D., Ingenito, A., Giacomazzi, E., et al.: Hydrogen/air supersonic combustion for future hypersonic vehicles. Int. J. Hydrogen Energy 36, 11969–11984 (2011)

78.

Chapuis, M., Fedina, E., Fureby, C., et al.: A computational study of the hyshot II combustor performance. Proc. Combust. Inst. 34, 2101–2109 (2013)

79.

Cocks, P.A.T.: Large eddy simulation of supersonic combustion with application to scramjet engines. [Ph.D. thesis]. Corpus Christi College, University of Cambridge (2011)

80.

Ingenito, A., Runo, C.B.: Mixing and combustion in supersonic reactive flows. In: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford, Connecticut, 21–23 July (2008)

81.

Ingenito, A., De Flora, M.G., Bruno, C.: LES modeling of scramjet combustion. In: 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, 9–12 January (2006)

82.

David, P., Graham, C.: Hybrid RANS/LES of a supersonic combustor. In: 26th AIAA Applied Aerodynamics Conference. Honolulu, Hawaii, 18–21 August (2008)

83.

Peterson, D.M., Candler, G.V., Drayna, T.W.: Detached eddy simulation of a generic scramjet inlet and combustor. In: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 5–8 January (2009)

84.

David, P., Erik, T., Graham, C.: Hybrid Reynolds-averaged and large-eddy simulation of scramjet fuel injection. In: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, California, 11–14 April (2011)

85.

Aksu, T., Uslu, S.: Large-eddy simulation of a dual-mode scramjet combustor using non-adiabatic flamelet modeling. In: 55th AIAA Aerospace Sciences Meeting. Grapevine, Texas, 9–13 January (2017)

86.

Zettervall, N., Fureby, C.: A computational study of ramjet, scramjet and dual-mode ramjet combustion in combustor with a cavity flameholder. In: 2018 AIAA Aerospace Sciences Meeting. Kissimmee, Florida, 8–12 January (2018)

87.

Kim, S.H., Donde, P., Raman, V., et al.: Large eddy simulation based studies of reacting and non-reacting transverse jets in supersonic crossflow. In: 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Nashville, Tennessee, 10 January (2012)

88.

Jung, C., Suresh, M.: Large-eddy simulation of cavity-stabilized supersonic combustion. In: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Denver, Colorado, 2–5 August (2009)

89.

Cai, Z., Wang, Z., Sun, M., et al.: Large eddy simulation of the flame propagation process in an ethylene fueled scramjet combustor in a supersonic flow. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China, 6–9 March (2017)

90.

Chaitanya, G., Jung, C., Srikant, S., et al.: Large eddy simulation of supersonic combustion in a cavity-strut flameholder. In: 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 4–7 January (2011)

91.

Jung, C., Chaitanya, G., Suresh, M.: Large-eddy simulation of cavity flame-holding in a Mach 2.5 cross flow. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 4–7 January (2010)

92.

Sun, M.B., Geng, H., Liang, J.H., et al.: Mixing characteristics in a supersonic combustor with gaseous fuel injection upstream of a cavity flameholder. Flow Turbul. Combust. 82, 271–286 (2008)MATH

93.

Gottiparthi, K.C., Sankaran, R., Ruiz, A.M., et al.: Large eddy simulation of a supercritical fuel jet in cross flow using GPU-acceleration. In: 54th AIAA Aerospace Sciences Meeting. San Diego, California, 4–8 January (2016)

94.

Gottiparthi, K.C., Sankaran, R., Oefelein, J.C.: High fidelity large eddy simulation of reacting supercritical fuel jet-in-cross-flow using GPU acceleration In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference. Salt Lake City, UT, 25–27 July (2016)

95.

Rajasekaran, A., Babu, V.: Numerical simulation of kerosene combustion in a dual mode supersonic combustor. In: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Sacramento, California, 9–12 July (2006)

96.

Behera, R., Chakraborty, D.: Numerical simulation of combustion in kerosene fueled ramp cavity based scramjet combustor. J. Aerospace Sci. Technol. 58, 104–111 (2006)

97.

Lacaze, G., Vane, Z., Oefelein, J.C.: Large eddy simulation of the hifire direct connect rig scramjet combustor. In: 55th AIAA Aerospace Sciences Meeting. Grapevine, Texas, 9–13 January (2017)

98.

Liu, Y., Dowling, A.P., Swaminathan, N., et al.: Prediction of noise source for an aeroengine combustor. In: 17th AIAA/CEAS Aeroacoustics Conference. Portland, Oregon, 5–8 June (2011)

99.

Clercq, P.L., Domenico, M.D., Rachner, M., et al.: Impact of fischer-tropsch fuels on aero-engine combustion performance. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 4–7 January (2010)

100.

Cazalens, M., Rullaud, M., Frenillot, J.P.: Computational methodology for carbon monoxide emission for aeroengine combustor design. J. Propul. Power 24, 779–787 (2008)

101.

Yang, J., Wu, X.Y., Wang, Z.G.: Parametric study of fuel distribution effects on a kerosene-based scramjet combustor. Int. J. Aerospace Eng. 7604279, 1–14 (2016)

102.

Dharavath, M., Manna, P., Sinha, P.K., et al.: Numerical analysis of a kerosene-fueled scramjet combustor. J. Therm. Sci. Eng. Appl. 8, 0110037 (2016)

103.

Zhang, M., Hu, Z., He, G., et al.: Large-eddy simulation of kerosene spray combustion in a model scramjet chamber. Proc. Inst. Mech. Eng. 224, 949–960 (2010)

104.

Kumaran, K., Behera, P.R., Babu, V.: Numerical investigation of the supersonic combustion of kerosene in a strut-based combustor. J. Propul. Power 26, 1084–1091 (2010)

105.

Zhang, M., Hu, Z., Luo, K.H., et al.: LES of kerosene spray combustion with pilot flame in a model dual mode ramjet chamber. In: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Denver, Colorado, 2–5 August (2009)

106.

Rajasekaran, A., Satishkumar, G., Babu, V.: Numerical simulation of the supersonic combustion of kerosene in a model combustor. Prog. Comput. Fluid Dyn. 9, 30–42 (2009)

107.

Rajasekaran, A., Babu, V.: Evaluation of a ramp cavity based concept supersonic combustor using CFD. Prog. Comput. Fluid Dyn. 9, 16–29 (2009)

108.

Kumaran, K., Babu, V.: Mixing and combustion characteristics of kerosene in a model supersonic combustor. J. Propul. Power 25, 583–592 (2009)

109.

Manna, P., Behera, R., Chakraborty, D.: Liquid-fueled strut-based scramjet combustor design: a computational fluid dynamics approach. J. Propul. Power 24, 274–281 (2008)

110.

Yamashita, H., Shimada, M., Takeno, T.: A numerical study on flame stability at the transition point of jet diffusion flames. Proc. Combust. Inst. 26, 27–34 (1996)

111.

Hartill, W.B.: Analytical and experimental investigation of a scramjet inlet of quadriform shape. U.S. Air Force Report No. AFAPL-TR-65-74, Marquardt Corporation (1965)

112.

Gruber, M., Smith, S., Mathur, T.: Experimental characterization of hydrocarbon-fueled, axisymmetric, scramjet combustor flowpaths. In: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, California, 11–14 April (2011)

113.

Smith, S., Gruber, M., Steiner, R., et al.: Development and calibration of an axisymmetric direct-connect supersonic-combustion flowpath. In: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Denver, Colorado, 2–5 August (2009)

114.

David, P., Russell, B., Vincent, W.: Hybrid Reynolds-averaged and large-eddy simulation of mixing in an axisymmetric scramjet. In: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. Tours, France, 24–28 September (2012)

115.

Houshang, E., Datta, G., Faure, M.M.: Exploratory RANS and LES simulations of transient supersonic combustor flow. In: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida, 5-8 January (2009)

116.

Doherty, L.J., Smart, M.K., Mee, D.J.: Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10. AIAA J. 53, 3196–3207 (2015)

117.

Suraweera, M.V., Smart, M.K.: Shock-tunnel experiments with a Mach 12 rectangular-to-elliptical shape-transition scramjet at offdesign conditions. J. Propul. Power 25, 555–564 (2009)

118.

Smart, M.K.: Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition. J. Propul. Power 17, 276–283 (2001)

119.

Gollan, R., Ferlemann, P.: Investigation of rest-class hypersonic inlet designs. In: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, California, 11–14 April (2011)

120.

Yue, W., Meneveau, C., Parlange, M.B., et al.: Turbulent kinetic energy budgets in a model canopy: comparisons between LES and wind-tunnel experiments. Environ. Fluid Mech. 8, 73–95 (2008)

Titel: Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms
verfasst von: Wei Yao
Publikationsdatum: 09.09.2019
Verlag: The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences
Erschienen in: Acta Mechanica Sinica / Ausgabe 6/2019
Print ISSN: 0567-7718
Elektronische ISSN: 1614-3116
DOI: https://doi.org/10.1007/s10409-019-00891-w

Premium Partner

Marktübersichten

Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.

Zur Marktübersicht

Springer Professional

Abstract

Bitte loggen Sie sich ein, um Zugang zu Ihrer Lizenz zu erhalten.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Weitere Artikel der Ausgabe 6/2019

Generalised energy conservation law for chaotic phenomena

Elastic property determination of nanostructured W/Cu multilayer films on a flexible substrate

Large deformation and wrinkling analyses of bimodular structures and membranes based on a peridynamic computational framework

Viscoelastic models revisited: characteristics and interconversion formulas for generalized Kelvin–Voigt and Maxwell models

DNS in evolution of vorticity and sign relationship in wake transition of a circular cylinder: (pure) mode A

Buckling-controlled two-way shape memory effect in a ring-shaped bilayer

Premium Partner

Marktübersichten