SCALING OF ROCKET NOZZLE ADMITTANCES

被引：7
|
作者：
JANARDAN, BA [1 ]
DANIEL, BR [1 ]
ZINN, BT [1 ]
机构：
[1] GEORGIA INST TECHNOL,SCH AEROSP ENGN,ATLANTA,GA 30332
来源：
AIAA JOURNAL | 1975年 / 13卷 / 07期
关键词：
D O I：
10.2514/3.60470
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：918 / 923
页数：6
相关论文
共 50 条
  • [41] Numerical simulation of flow separation in rocket nozzle
    Hadjadj, A
    Nebbache, A
    Vuillamy, D
    Vandromme, D
    MECHANICS RESEARCH COMMUNICATIONS, 1997, 24 (03) : 269 - 276
  • [42] CAD system of solid rocket motor nozzle
    Xu, Xu
    Yang, Li
    Zhang, Zhenpeng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 1996, 11 (04): : 373 - 376
  • [43] RELATIONSHIP OF GRAPHITE PROPERTIES TO ROCKET NOZZLE EROSION
    SLOSARIK, SE
    SWOPE, LM
    CARBON, 1964, 1 (03) : 358 - 358
  • [44] On the characterization of methane in rocket nozzle cooling channels
    Heldens, Jules C.
    Fridh, Jens
    Ostlund, Jan
    ACTA ASTRONAUTICA, 2021, 186 : 337 - 346
  • [45] Simulation of a Rocket Engine Nozzle Discharge Coefficient
    Sabirzyanov A.N.
    Glazunov A.I.
    Kirillova A.N.
    Titov K.S.
    Russian Aeronautics, 2018, 61 (02): : 257 - 264
  • [46] SCALING LAWS FOR CONDENSATION IN NOZZLE FLOWS
    HAGENA, OF
    PHYSICS OF FLUIDS, 1974, 17 (05) : 894 - 896
  • [47] Novell application of CFD for rocket engine nozzle optimization
    Jéger C.
    Veress Á.
    Periodica Polytechnica Transportation Engineering, 2019, 47 (02): : 131 - 135
  • [48] FLOW THROUGH A ROCKET NOZZLE WITH AND WITHOUT VIBRATIONAL EQUILIBRIUM
    PENNER, SS
    JOURNAL OF APPLIED PHYSICS, 1949, 20 (05) : 445 - 447
  • [49] ABLATIVE ROCKET-NOZZLE DESIGN FOR EARTH ENTRY
    SVENSON, FC
    SIMKIN, DJ
    FISHER, MW
    MECHANICAL ENGINEERING, 1966, 88 (07) : 70 - &
  • [50] COMPARISON OF METHODS FOR THE CALCULATION OF ROCKET NOZZLE WALL TEMPERATURES
    SCHOYER, HFR
    AIAA JOURNAL, 1980, 18 (07) : 841 - 842
12345