期刊文献+

火箭发动机羽流红外特性研究概述 被引量:5

Review of Research on Infrared Radiation Signatures of Rocket Exhaust Plume
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摘要 介绍了国内外火箭发动机羽流红外特性的研究进展及实验研究方法,总结了计算发动机羽流红外特性常用的求解方法及其特点,提出国内应当在辐射模型的完善及与流场计算的耦合度、高空辐射模型的建立、实验数据获取等方面开展更深入的研究工作。 The situation of international and domestic research on the infrared (IR) radiation signatures of rocket exhaust plume is briefly introduced. The commonly solutions and their characteristics for the IR signatures of rocket exhaust plume are summarized. It is pointed out that more research works should be done in the fields such as the radiation model optimization, the coupling of the radiation calculation and flow field simulation, the high altitude radiation model building and valuable measurement data acquirement.
出处 《导弹与航天运载技术》 北大核心 2009年第5期18-21,25,共5页 Missiles and Space Vehicles
基金 国防基础预研项目资助(B2220060060)
关键词 火箭发动机 羽流 红外辐射 数值模拟 Rocket motor Exhaust plume Infrared radiation Numerical simulation Experimental study
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参考文献35

  • 1Ludwing C B, Malkmus W, Reardon J E, et al. Handbook of infrared radiation from combustion gases[R]. NASA-SP-3080, 1973.
  • 2Hermsen R W. Aluminum oxide particle size for solid rocket motor performance prediction [J]. Journal of Spacecraft & Rockets, 1981, 18(6):483-490.
  • 3Gosse S, Hespel L, Gossart, et al. Morphological characterization and particle sizing of alumina particles in solid rocket motor [J]. Journal of Propulsion and Power, 2006, 22(1):127-135.
  • 4Konopka W L, Reed R A, Calia V S. Measurements of infrared optical properties of Al2O3 rocket particles[R]. AIAA-83-1568, 1983.
  • 5Reed R A, Calia V S. Review of aluminum oxide rocket exhaust particles[R]. AIAA-93-2819, 1993.
  • 6Freeman G N, Ludwig C B, Malkmus W, et al. Development and validation of standardized infrared radiation model (SIRRM) [R]. AFRPL-79-55, 1979.
  • 7Surzhikov S T. Direct simulation Monte-Carlo algorithms for the rocket exhaust plumes emissivity prediction[R]. AIAA-2002-0795, 2002.
  • 8Everson J, Nelson H F. Rocket plume radiation base heating by reverse Monte Carlo simulation [J]. Journal of Thermophysics and Heat Transfer, 1993, 7(4):717-723.
  • 9Burt J M, Boyd I D. A Monte Carlo radiation model for simulating rarefied multiphase plume flows[R]. AIAA-2005-4691, 2005.
  • 10Kim M Y, Yu M J, Cho J H, et al. Influence of particles on radiative base heating from the rocket exhaust plume[J]. Journal of Spacecraft and Rockets, 2008, 45(3):454-458.

二级参考文献62

  • 1周英彪,阮立明,李剑云,郑楚光.不同燃尽程度下粉煤燃烧微粒的光学特性和辐射特性[J].电站系统工程,1995,11(4):51-55. 被引量:2
  • 2徐南荣.喷气流红外辐射场的数值计算[J].航空学报,1995,16(6):647-653. 被引量:20
  • 3刘林华,余其铮,阮立明,谈和平.煤、灰粒子的辐射特性[J].燃烧科学与技术,1996,2(2):127-133. 被引量:6
  • 4董土奎.[D].哈尔滨:哈尔滨工业大学,2002.
  • 5阮立明.[D].哈尔滨:哈尔滨工业大学,1997.
  • 6蔡国飙,王慧玉,祖国君,张振鹏.真空小喷管羽流场的Monte Carlo直接模拟[J].推进技术,1997,18(2):44-49. 被引量:11
  • 7[1]Ludwing C B, Malkmus W, Walker J, et al. A theoretical model for absorbing, emitting and scattering plume radiation. Horton T E (Ed). Spacecraft Radative Transfer and Temperature Control. New York: AIAA Progress Series in Astronautics and Aeronautics, 1982, 83: 111-127
  • 8[4]Piesik E T. Aluminized propellants and a method defining low-altitude exhaust plumes. J. of Spacecraft and Rocket, 1986, 23: 215-221
  • 9[5]Scutaru D. Measurements and calculations of CO2 absorption at high temperature in the 4.3 and 2.7μm regions. J.of Quantitative Spectroscopy and Radiative Transfer, 1993, 50(2): 179-191
  • 10[8]Thompson J F, Warsi U A, Masin C W. Numerical grid generation: Foundations and applications. New York: North-Holland, 1985,95-169

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引证文献5

二级引证文献17

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