Effect of a blocked channel on the wall temperature of a regeneratively cooled rocket thrust chamber

被引:0
|
作者
Naraghi, Mohammad H. [1 ]
Quentmeyer, Richard J. [2 ]
Mohr, David H. [3 ]
机构
[1] Department of Mechanical Engineering, Manhattan College, Riverdale NY 10471, United States
[2] 2703 Country Club Blvd, Rocky River, OH 44116, United States
[3] D and E Propulsion and Power Systems, 3840 Hammock Rd, Mims, FL 32754, United States
关键词
D O I
July 8, 2001 - July 11, 2001
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 45 条
  • [21] Improved Wall Temperature Prediction for the LUMEN Rocket Combustion Chamber with Neural Networks
    Dresia, Kai
    Kurudzija, Eldin
    Deeken, Jan
    Waxenegger-Wilfing, Guenther
    AEROSPACE, 2023, 10 (05)
  • [22] EDDY VISCOSITY CALCULATION ALONG CHEMICAL ROCKET THRUST CHAMBER WALL USING TURBULENT KINETIC-ENERGY
    OMORI, S
    COMBUSTION SCIENCE AND TECHNOLOGY, 1973, 7 (06) : 229 - 240
  • [23] Research on Cooling Effect with Cooling Groove Structure Parameters of Liquid Rocket Engine Thrust Chamber
    Nie, Tao
    Liu, Weiqiang
    MECHANICAL ENGINEERING AND MATERIALS SCIENCE, 2012, 108 : 7 - 11
  • [24] EFFECT OF LOW-STIFFNESS CLOSEOUT OVERWRAP ON ROCKET THRUST-CHAMBER LIFE.
    Kasper, Harold J.
    Notardonato, J.Joseph
    NASA Technical Paper, 1979, (1456):
  • [25] Numerical simulation and optimization on heat transfer and fluid flow in cooling channel of liquid rocket engine thrust chamber
    Wang, Qiuwang
    Wu, Feng
    Zeng, Min
    Luo, Laiqin
    Sun, Jiguo
    ENGINEERING COMPUTATIONS, 2006, 23 (7-8) : 907 - 921
  • [26] Damage-mitigating control of a reusable rocket engine .1. Life prediction of the main thrust chamber wall
    Dai, XW
    Ray, A
    JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 1996, 118 (03): : 401 - 408
  • [27] ONE-DIMENSIONAL, STEADY FLOW WITH MASS ADDITION AND THE EFFECT OF COMBUSTION CHAMBER FLOW ON ROCKET THRUST
    PRICE, EW
    JET PROPULSION, 1955, 25 (02): : 61 - 66
  • [28] EFFECT OF 2-DIMENSIONAL HEAT TRANSFER ON WALL TEMPERATURES IN A TUBULAR THRUST CHAMBER
    SELLERS, JP
    ARS JOURNAL, 1961, 31 (03): : 445 - 447
  • [29] The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines
    Zhou, Chuang
    Yu, Nanjia
    Wang, Shuwen
    Han, Shutao
    Gong, Haojie
    Cai, Guobiao
    Wang, Jue
    AEROSPACE, 2023, 10 (01)
  • [30] THE EFFECT OF DISCHARGE CHAMBER WALL TEMPERATURE ON ION-THRUSTER PERFORMANCE
    WILBUR, PJ
    BROPHY, JR
    AIAA JOURNAL, 1986, 24 (02) : 278 - 283