Choked gas flow through nozzles: An explicit formula for the inlet Mach number

被引:1
|
作者
Morris, SD
机构
[1] Process Engineering Unit, TP 250, Joint Research Centre (Ispra), European Commission, 21020 Ispra, Varese
关键词
choked gas flow; nozzle inlet; Mach number;
D O I
10.1016/0950-4230(96)00006-X
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
A simple analytical formula is derived for the inlet Mach number of an ideal nozzle through which there is choked flow of gas. This formula, valid for diameter ratios beta less than or equal to 0.99, permits the explicit calculation of choked flow parameters to an accuracy <0.1%, thus offering simplicity in comparison to existing iterative methods. The formula has application in the area of pressure relief system design. Copyright (C) 1996 Elsevier Science Ltd
引用
收藏
页码:189 / 191
页数:3
相关论文
共 50 条
  • [1] Choked gas flow through pipeline restrictions: An explicit formula for the inlet Mach number
    Morris, SD
    JOURNAL OF HAZARDOUS MATERIALS, 1996, 50 (01) : 71 - 77
  • [2] A MODEL FOR CHOKED FLOW-THROUGH CRACKS WITH INLET SUBCOOLING
    FEBURIE, V
    GIOT, M
    GRANGER, S
    SEYNHAEVE, JM
    INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 1993, 19 (04) : 541 - 562
  • [3] DISCHARGE COEFFICIENTS FOR CHOKED GAS-LIQUID FLOW THROUGH NOZZLES AND ORIFICES AND APPLICATIONS TO SAFETY DEVICES
    MORRIS, SD
    JOURNAL OF LOSS PREVENTION IN THE PROCESS INDUSTRIES, 1990, 3 (03) : 303 - 310
  • [4] NUMERICAL-SOLUTION OF CHOKED AND SUPERCRITICAL IDEAL-GAS FLOW THROUGH ORIFICES AND CONVERGENT CONICAL NOZZLES
    ALDER, GM
    JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 1979, 21 (03): : 197 - 203
  • [5] Effect of inlet Mach number on performance and flow structure of an axial supersonic through-flow fan cascade
    Sun, Shijun
    Li, Xiaolong
    Guo, Minghao
    Song, Jinyu
    Yang, Ce
    Wang, Jianhua
    PHYSICS OF FLUIDS, 2023, 35 (05)
  • [6] EXTENSION OF ONE-DIMENSIONAL THEORY TO INVISCID SWIRLING FLOW THROUGH CHOKED NOZZLES
    CARPENTER, PW
    JOHANNESEN, NH
    AERONAUTICAL QUARTERLY, 1975, 26 (MAY): : 71 - 87
  • [7] Experimental investigation of effects of mach number on the flow instability in a supersonic inlet
    M. R. Soltani
    M. Farahani
    Experimental Techniques, 2013, 37 : 46 - 54
  • [8] Experimental Investigation of Effects of Mach Number on the Flow Instability in a Supersonic Inlet
    Soltani, M. R.
    Farahani, M.
    EXPERIMENTAL TECHNIQUES, 2013, 37 (03) : 46 - 54
  • [9] Choked Flow Characteristics of Subcritical Refrigerant Flowing Through Converging-Diverging Nozzles
    Zhang, Zhenying
    Tian, Lili
    Tong, Lirui
    Chen, Yanhua
    ENTROPY, 2014, 16 (11): : 5810 - 5821
  • [10] Real-Gas Effects on Hypersonic Inlet Flow at Mach 10
    Zhang Q.-F.
    Yue L.-J.
    Jia Y.-N.
    Zhang X.-Y.
    Li X.
    Gao X.
    Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (05): : 1042 - 1050