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  1. No Access

    Article

    DDT and detonation waves in dust-air mixtures

    This paper summarizes the studies of DDT and stable detonation waves in dust-air mixtures at the Stosswellenlabor of RWTH Aachen. The DDT process and propagation mechanism for stable heterogeneous dust detona...

    F. Zhang, H. Grönig, A. van de Ven in Shock Waves (2001)

  2. No Access

    Article

    Detonation formation in H $_2$-O $_2$/He/Ar mixtures at elevated initial pressures

    In this paper the formation of detonation in H \(_2\) -O \(_2\) /He/Ar mixtures at elevated initial pressures was investigated in an initiation t...

    B.L. Wang, M. Habermann, M. Lenartz, H. Olivier, H. Grönig in Shock Waves (2000)

  3. No Access

    Article

    Detonation and deflagration initiation at the focusing of shock waves in combustible gaseous mixture

    B.E. Gelfand, S.V. Khomik, A.M. Bartenev, S.P. Medvedev, H. Grönig in Shock Waves (2000)

  4. No Access

    Article

    Effect of reflection type on detonation initiation at shock-wave focusing

    A.M. Bartenev, S.V. Khomik, B.E. Gelfand, H. Grönig, H. Olivier in Shock Waves (2000)

  5. No Access

    Article

    Pressure measurements on cone surface in 3-D shock reflection processes

    In a shock tube the pressure distribution was measured on a cone with an angle of attack when a shock wave passed the cone. The cone has a semi-apex angle of 35°, the angle of attack varied from 0° to 25° and...

    H. Zhao, X.Z. Yin, H. Grönig in Shock Waves (1999)

  6. No Access

    Article

    Microwave detection of molecules formed by shock wave induced reactions

    The paper describes experimental investigations in a shock tube concerning the formation of new molecules using He as a driver gas and a mixture of Kr, CH \(_4\) and NH ...

    D. Ewert, H. Grönig, H. Olivier, W. Stahl, E. Sedlmayr, D. Zimmermann in Shock Waves (1998)

  7. No Access

    Article

    Behavior of detonation waves at low pressures

    With respect to stability of gaseous detonations, unsteady behavior of gallo** detonations and re-initiation process of hydrogen-oxygen mixtures are studied using a detonation tube of 14 m in length and 45 ...

    K. Ishii, H. Grönig in Shock Waves (1998)

  8. No Access

    Article

    Shock waves from an open-ended shock tube with different shapes

    A new method for decreasing the attenuation of a shock wave emerging from an open-ended shock tube exit into a large free space has been developed to improve the shock wave technique for cleaning deposits on t...

    Q. Yu, H. Grönig in Shock Waves (1996)

  9. No Access

    Chapter and Conference Paper

    Numerical Simulation of the Interaction of a Shock Wave with a Two-Phase Interface

    The one-dimensional unsteady flow field induced by a planar incident shock wave propagating into a gas-particle mixture without chemical reactions has been calculated using the PLM-algorithm based on the high-...

    Q. Yu, A. van de Ven, J. H. Geng, F. Zhang, H. Grönig in Shock Waves @ Marseille III (1995)

  10. No Access

    Chapter and Conference Paper

    Six-Component Force Measurement in the Aachen Shock Tunnel

    A six-component strain-gauge balance for short-duration hypersonic facilities is presented. The balance features a new geometry compared to classical strain-gauge balances for model measurements in wind tunnel...

    C. Jessen, H. Grönig in Shock Waves @ Marseille I (1995)

  11. No Access

    Chapter and Conference Paper

    Navier-Stokes Simulation and Measurement of Cone Drag at M = 7.9

    The calculation of a M = 7.9 flow around a 30° cone in a shock tunnel is presented. It starts from the initial reservoir conditions obtained in the experiment in fr...

    C. Jessen, H. Grönig, M. Watanabe, K. Takayama in Shock Waves @ Marseille I (1995)

  12. No Access

    Chapter and Conference Paper

    Shock Wave Diffraction — New Aspects of an Old Problem

    The classical gas dynamics problem of a shock wave diffracting at a sharp 90° corner is investigated both numerically and experimentally. Recent improvements of the visualization techniques and a high-resoluti...

    H. Kleine, E. Ritzerfeld, H. Grönig in Shock Waves @ Marseille IV (1995)

  13. No Access

    Chapter and Conference Paper

    Experiments and Model Computation of Cylindrical Shock Waves with Time-Resolved Deformation and Fragmentation

    Since real converging shock waves are not perfectly symmetric at least a two-dimensional description of their properties is necessary, as can be seen, e.g., from the experiments of K. Takayama, H. Kleine and H...

    F. Demmig, H. Grönig, H. Kleine, H. Wallus in Shock Waves @ Marseille IV (1995)

  14. No Access

    Article

    Specific features of incident and reflected blast waves

    On the basis of numerical modeling specific features of shock wave reflections were analyzed. It was found, that after diaphragm rupture self-modeling pressure and velocity distributions nearby the shock front...

    B. E. Gelfand, A. M. Bartenev, S. P. Medvedev, A. N. Polenov, S. V. Khomik in Shock Waves (1994)

  15. No Access

    Article

    Interaction of a shock wave with a two-phase interface

    The acceleration by an incident shock of a planar interface between a gas and a particle-gas mixture has been investigated experimentally and numerically. The experiments were conducted in a newly developed ve...

    J. H. Geng, A. van de Ven, Q. Yu, F. Zhang, H. Grönig in Shock Waves (1994)

  16. No Access

    Article

    Time integration method to determine the characteristic parameter of a light extinctiometer

    The linear relation between the particle concentration and the output voltage of a light extinctiometer used to measure particle concentrations has been derived and calibrated. A time integration method was in...

    J. H. Geng, A. van de Ven, F. Zhang, H. Grönig in Experiments in Fluids (1993)

  17. No Access

    Chapter

    Measurements on Models for Hypersonic Real Gas Conditions

    Pressure and particularly heat transfer measurements on the surface of a model in the test section flow of a shock tunnel are discussed. The heat transfer gauges include thin films, thermocouples and calorimet...

    H. Olivier, M. Vetter, C. Jessen, H. Grönig in New Trends in Instrumentation for Hyperson… (1993)

  18. No Access

    Chapter

    A Six Component Balance for Short Duration Hypersonic Facilities

    A new balance for six component forces measurements in short duration hypersonic facilities is presented. Construction and functioning of the system are described in detail. The third order calibration is expl...

    C. Jessen, H. Grönig in New Trends in Instrumentation for Hypersonic Research (1993)

  19. No Access

    Article

    Gaseous detonation driver for a shock tunnel

    The concept of a shock tunnel with gaseous detonation driver is discussed. A detonation driver presents an alternative to a free-piston driver because comparable values of high enthalpy can be attained, howeve...

    H. -r. Yu, B. Esser, M. Lenartz, H. Grönig in Shock Waves (1992)

  20. No Access

    Article

    Propagation mechanism of dust detonations

    This paper summarizes the studies on dust detonations at the Stosswellenlabor of RWTH Aachen since 1987. The onset and propagation mechanism of heterogeneous dust detonations are similar to those of marginal g...

    F. Zhang, P. Greilich, H. Grönig in Shock Waves (1992)

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