The use of driver inserts to reduce non-ideal pressure variations behind reflected shock waves

被引:98
|
作者
Hong, Zekai [1 ]
Pang, Genny A. [1 ]
Vasu, Subith S. [1 ]
Davidson, David F. [1 ]
Hanson, Ronald K. [1 ]
机构
[1] Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
关键词
TUBE FLOWS; TIME; TEMPERATURE; MIXTURES; MODEL;
D O I
10.1007/s00193-009-0205-y
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Non-ideal shock tube facility effects, such as incident shock wave attenuation, can cause variations in the pressure histories seen in reflected shock wave experiments. These variations can be reduced, and in some cases eliminated, by the use of driver inserts. Driver inserts, when designed properly, act as sources of expansion waves which can counteract or compensate for gradual increases in reflected shock pressure profiles. An algorithm for the design of these inserts is provided, and example pressure measurements are presented that demonstrate the success of this approach. When these driver inserts are employed, near- ideal, constant-volume performance in reflected shock wave experiments can be achieved, even at long test times. This near-ideal behavior simplifies the interpretation of shock tube chemical kinetics experiments, particularly in experiments which are highly sensitive to temperature and pressure changes, such as measurements of ignition delay time of exothermic reactions.
引用
收藏
页码:113 / 123
页数:11
相关论文
共 50 条
  • [1] The use of driver inserts to reduce non-ideal pressure variations behind reflected shock waves
    Zekai Hong
    Genny A. Pang
    Subith S. Vasu
    David F. Davidson
    Ronald K. Hanson
    Shock Waves, 2009, 19 : 113 - 123
  • [2] Non-ideal oblique shock waves
    Vimercati, Davide
    Gori, Giulio
    Guardone, Alberto
    JOURNAL OF FLUID MECHANICS, 2018, 847 : 266 - 285
  • [3] Propagation of Weak Shock Waves in a Non-Ideal Gas
    Singh, Lal. P.
    Singh, Dheerendra. B.
    Ram, Subedar
    OPEN ENGINEERING, 2011, 1 (03): : 287 - 294
  • [4] Similarity Solutions to Shock Waves in Non-Ideal Magnetogasdynamics
    Dunna, Narsimhulu
    Ramu, Addepalli
    Satpathi, Dipak Kumar
    11TH INTERNATIONAL CONFERENCE OF NUMERICAL ANALYSIS AND APPLIED MATHEMATICS 2013, PTS 1 AND 2 (ICNAAM 2013), 2013, 1558 : 860 - 864
  • [5] Evolution of weak shock waves in non-ideal magnetogasdynamics
    Amin, Danish
    Singh, Dheerendra B.
    ZEITSCHRIFT FUR NATURFORSCHUNG SECTION A-A JOURNAL OF PHYSICAL SCIENCES, 2022, 77 (09): : 829 - 839
  • [6] Evolution of weak shock waves in non-ideal magnetogasdynamics
    Nath, Triloki
    Gupta, R. K.
    Singh, L. P.
    ACTA ASTRONAUTICA, 2017, 133 : 397 - 402
  • [7] Propagation of strong shock waves in a non-ideal gas
    Tomar, Amit
    Arora, Rajan
    Chauhan, Antim
    ACTA ASTRONAUTICA, 2019, 159 : 96 - 104
  • [8] Convergence of strong shock waves in non-ideal magnetogasdynamics
    Chauhan, Antim
    Arora, Rajan
    Tomar, Amit
    PHYSICS OF FLUIDS, 2018, 30 (11)
  • [9] Parameters of pressure waves in case of non-ideal explosions
    Izv Akad Nauk Mekh Zhidk Gaza, 1600, 5 (132-150):
  • [10] Similarity solutions for the flow behind an exponential shock in a non-ideal gas
    J. P. Vishwakarma
    G. Nath
    Meccanica, 2007, 42 : 331 - 339