Abstract
A shock wave which is incident onto a gas-particle mixture or initiated within such a mixture needs a certain distance to reach a constant velocity. This effect is due to the inertia and the heat capacity of the particles. In general the shock wave is decelerated and the frozen pressure jump is decaying.
A vertical shock tube was used in order to produce a plane shock wave incident onto a homogeneous gas-particle mixture. In addition to measurements of the shock velocity and the pressure history along the total low pressure section, the particle velocity was measured within the relaxation zone far downstream of the diaphragm using a laser-Doppler-velocimeter. Thus a drag law describing the particle acceleration within the relaxation zone was derived from the measurements.
To compare the experiments with theoretical results, calculations were performed by the random-choice method.
Similar content being viewed by others
Abbreviations
- a :
-
velocity of sound
- c :
-
specific heat of particles
- c p :
-
specific heat of the gas at constant pressure
- c v :
-
specific heat of the gas at constant volume
- c D :
-
drag coefficient
- D p :
-
particle diameter
- F p :
-
drag force
- m p :
-
particle flow rate
- m G :
-
gas flow rate
- \(Ms = \frac{{u_s }}{{a_1 }}\) :
-
shock Mach number
- M s0 :
-
initial shock Mach number
- Nu :
-
Nusselt number
- p :
-
pressure
- Pr :
-
Prandtl number
- Q p :
-
heat transfer
- R :
-
gas constant
- Re :
-
Reynolds number
- t :
-
time
- T :
-
temperature
- u :
-
flow velocity
- u s :
-
shock wave velocity
- χ:
-
coordinate
- γ:
-
ratio of the specific heats of the gas
- δ:
-
ratio of the specific heats of the particles and the gas
- ɛ:
-
volume fraction of the particles
- ν:
-
loading ratio
- μ:
-
dynamic viscosity
- ϱ:
-
gas density
- ϱ p :
-
density of particle material
- σ:
-
particle density in the mixture
- E :
-
equilibrium
- e :
-
equivalent gas
- G :
-
gas
- P :
-
particles
References
Chorin, A. J. 1976: Random choice solution of hyperbolic systems. J. Comp. Phys. 22, 517–533
Ford, C. A.; Glass, I. I. 1954: An experimental study of shock wave refraction. UTIA Rep. No. 29
Higashino, F. 1983: Characteristics method applied to blast waves in a dusty gas. Z. Naturforsch. 38 a, 399–406
Ingebo, R. D. 1956: Drag coefficient for droplets and solid spheres in clouds accelerating in air streams. NACA TN 3762
Knudsen, J. G.; Katz, D. L. 1958: Fluid Mechanics and Heat Transfer, pp. 511. New York: McGraw-Hill
Levine, A. S. 1971: A theoretical analysis of unsteady supersonic gas-particle suspension flows using the Particle-In-Cell method. Ph.D. Thesis, Northeastern University Boston, Massachusetts
Marble, F. E. 1970: Dynamics of dusty gases. Ann. Rev. Fluid Mech. 2, 397–446
Marconi, F.; Rudman, S.; Calia, V. 1981: Numerical study of one dimensional unsteady particle-laden flows with shock. AIAA J. 19, 1294–1301
Miura, H.; Glass, I. I. 1981: On a study-gas shock tube. UTIAS Rep. No. 250
Outa, E.; Tajima, K.; Morii, H. 1976: Experiments and analysis on shock wave propagation through a gas-particle-mixture. Bull. JSME 19, 384–394
Outa, E.; Tajima, K.; Suzuki, S. 1981: Cross-sectional concentration of particles during shock process propagating through a gas-particle mixture in a shock tube. Proc. 13th Int. Symp. on Shock Tubes and Waves (Ed. Treanor, C. E.; Hall, J. G.), pp. 655–663. Albany, New York: State University of New York Press
Rudinger, G. 1964: Some properties of shock relaxation in gas flows carrying small particles. Phys. Fluids 7, 658–663
Rudinger, G.; Chang, A. 1964: Analysis of nonsteady two phase flow. Phys. Fluids 7, 1747–1754
Rudinger, G. 1970: Effective drag coefficient for gas-particle flow in shock tubes. Trans. ASME, J. Bas. Eng. 92, 165–172
Rudinger, G. 1965: Some effects of finite volume on the dynamics of gas-particle mixtures. AIAA J. 3, 1217–1222
Saito, T.; Glass, I. 1. 1979: Application of random choice method to problems in shock and detonation wave dynamics. UTIAS Rep. No. 240
Satofuka, N.; Tokita, K. 1979: Finite difference calculation of gas-particle flows in shock tubes. Mem. Fac. Ind. Arts, Kyoto Techn. Univ. 28, 28–39
Schmitt-v. Schubert, B. 1970: Struktur stationarer Verdichtungsstöße in Gasen mit festen Teilchen ZAMM 50, 671–682
Smeets, G.; George, A. 1980: Laser-Doppler-Velozimeter mit einem Michelson-Spektrometer. ISL Bericht R 109/80
Sommerfeld, M.; Grönig, H. 1983 a: Grenzschichten in Gas-Teilchen-Strömungen hinter Stoßwellen. Forschungsbericht des Landes NRW Nr. 3171
Sommerfeld, M.; Grönig, H. 1983 b: Decay of shock waves in a dusty gas shock tube with different configurations. Proc. 14th Int. Symp. on Shock Tubes and Waves (Ed. Archer, R. D.; Milton, B. E.). Sydney Shock Tube Symposium Publishers
Sommerfeld, M. 1984: Instationäre Stoßwellenausbreitung in Gas-Teilchen-Gemischen. Diss., RWTH Aachen
Varma, T. D.; Chopra, N. K. 1967: Analysis of normal shock waves in a gas-particle mixture. ZAMP 18, 650–660
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Sommerfeld, M. The unsteadiness of shock waves propagating through gas-particle mixtures. Experiments in Fluids 3, 197–206 (1985). https://doi.org/10.1007/BF00265101
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF00265101