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Experimental investigation of hypersonic flow induced separation over double wedges

Journal of Thermal Science 2009年第3期18卷 220-225页

作者： Tokitada Hashimoto Saga University

Flow separation occurs over the compression comers generated by deflected control surfaces on hypersonic re-entry vehicles and in the inlet of scram jet engines. Configurations like a double wedge and double cone model are useful for studying the separated flow features. Flow fields around concave comers are relatively complicated and produce several classical viscous flow features depending on the combination of the first and second wedge or cone half apex angles. Particularly characteristic phenomena are mainly shock/boundary layer, shock/shock interaction, unsteady shear layers and non-linear shock oscillations. Although most of these basic gas dynamics characteristics are well known, it is not clear what happens at high enthalpy conditions. This paper reports a result of flow fields over a double wedge at a stagnation enthalpy of 4.8 MJ/kg. The experiment was carried out in a free piston shock tunnel at a nominal Mach number of 6.99. Schlieren and double exposure holographic interferometry were applied to visualize the flow field over the double wedge.

关键词： double wedge separation shock interaction

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Investigation of strong shock wave interactions with CeO2 ceramic

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Journal of Advanced Ceramics 2014年第4期3卷 297-305页

作者： Vishakantaiah JAYARAM Asha GUPTA K.P.J.REDDY shock Induced Materials Chemistry Lab SSCUIndian Institute of ScienceBangalore-560012India Texas Materials Institute the University of Texas at AustinAustinTexas 78712USA Department of Aerospace Engineering Indian Institute of ScienceBangalore-560012India

Strong shock wave interactions with ceramic material ceria(CeO_(2))in presence of O_(2)and N2 gases were investigated using free piston driven shock tube(FPST).FPST is used to heat the test gas to very high temperature of about 6800-7700 K(estimated)at pressure of about 6.8-7.2 MPa for short duration(2-4 ms)behind the reflected shock *** is subjected to super heating and cooling at the rate of about 106 K/*** of CeO_(2)sample was done before and after exposure to shock heated test gases(O_(2)and N2).The surface composition,crystal structure,electronic structure and surface morphology of CeO_(2)ceramic were examined using X-ray photoelectron spectroscopy(XPS),X-ray diffraction(XRD),Fourier transform infrared(FTIR)spectrometry,scanning electron microscopy(SEM)and high resolution transmission electron microscopy(HRTEM).Results obtained from the experimental investigations show that CeO_(2)can withstand high pressure accompanied by thermal shock without changing its crystal *** CeO_(2)releases lattice oxygen making it possible to shift between reduced and oxidized states upon the interaction with shock heated *** to such reaction mechanism,CeO_(2)ceramic undergoes nitrogen doping with decrease in lattice *** reveal that CeO_(2)retains its crystal structure during strong shock interaction,even at elevated pressure.

关键词： shock tube shock interaction high enthalpy gas ceria nitrogen-doped surface reaction

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On transition of type V interaction in double-wedge flow with non-equilibrium effects

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Theoretical & Applied Mechanics Letters 2016年第6期6卷 282-285页

作者： Wentao Xiong Yujian Zhu Xisheng Luo Advanced Propulsion Laboratory Department of Modern MechanicsUniversity of Science and Technology of China

The transition between regular reflection （RR） and Mach reflection （MR） of type V shock-shock interaction on a double-wedge geometry with high temperature non-equilibrium effects is investigated by extended shock-polar method and numerical simulation. First, the critical angles of transition from detachment criterion and yon Neumann criterion are determined by the extended shock-polar method considering the non-equilibrium effects. Then wave patterns and the transition process are numerically obtained. Results of the critical transition angles from shock-polar calculation and numerical simulation show evident disagreement, indicating transition mechanism between RR and MR of type V interaction is changed. By comparing with the frozen counterpart, it is also found that non-equilibrium effects lead to a larger critical wedge angle and a larger hysteresis interval.

关键词： shock interaction Non-equilibrium effects shock polar Hypersonic flow

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