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Study of shock-shock interactions for the HET facility double wedge configuration using the DSMC approach

Patil, V. N. and Levin, D. A. and Gimelshein, S. G. and Austin, J. M. (2013) Study of shock-shock interactions for the HET facility double wedge configuration using the DSMC approach. In: 43rd AIAA fluid dynamics conference and exhibit 2013. AIAA , Red Hook, NY. ISBN 9781627488914. http://resolver.caltech.edu/CaltechAUTHORS:20140924-131045732

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Abstract

A set of numerical simulations designed to study the laminar, shock-shock interactions from hypersonic flows about a double-wedge configuration for the Hypervelocity Expansion Tube (HET) facility are presented. Computations are made using the Direct Simulation Monte Carlo (DSMC) method, an approach for modeling finite-Knudsen number flows. The current study focuses on the investigation of Mach 7 nitrogen flows about a 30-/55-deg double wedge model for stagnation enthalpies varying from 2.0-8.0 MJ/kg. The simulation results of the double wedge flows are compared with the data obtained from experiments at HET. Numerical Schlierens are generated to visualize the shock structure and shock-shock interactions present in these flows and are compared with the experimental Schlieren images. The computed heat transfer values from the simulations match the experiment along the first surface, but on the second wedge the computed heat transfer distribution over predicts the measured peak values. The influence of different models for nonequilibrium nitrogen dissociation, rotational and vibrational relaxation rates, and gas-surface interactions on the shock interaction region are analyzed for high enthalpy flow features and heat transfer rates. Overall good agreement is observed in the experimental and computational results. Unsteadiness of the flow and time-averaging of the experimental measurements are likely reasons for the inability of the DSMC simulations to exactly reproduce the experimental data.


Item Type:Book Section
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http://arc.aiaa.org/doi/abs/10.2514/6.2013-3202PublisherAbstract
http://dx.doi.org/10.2514/6.2013-3202DOIAbstract
Additional Information:© 2013 by the American Institute of Aeronautics and Astronautics, Inc. AIAA 2013-3202. The research performed at the Pennsylvania State University was supported by the Air Force Office of Scientific Research through AFOSR Grant No. FA9550-11-1-0129 with a subcontract award number 2010-06171-01 to PSU. We would like to acknowledge Prof. M. Ivanov of the Institute of Theoretical and Applied Mechanics, Russia for the use of the original SMILE code.
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)FA9550-11-1-0129
UNSPECIFIED2010-06171-01
Record Number:CaltechAUTHORS:20140924-131045732
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20140924-131045732
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:49998
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:29 Sep 2014 21:52
Last Modified:20 Sep 2016 23:10

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