THERMAL SCIENCE

International Scientific Journal

NUMERICAL ANALYSIS OF A HYPERSONIC TURBULENT AND LAMINAR FLOW USING A COMMERCIAL CFD SOLVER

ABSTRACT
Computational fluid dynamics computations for two hypersonic flow cases using the commercial ANSYS FLUENT 16.2 CFD software were done. In this paper, an internal and external hypersonic flow cases were considered and analysis of the hypersonic flow using different turbulence viscosity models available in ANSYS FLUENT 16.2 as well as the laminar viscosity model were done. The obtained results were after compared and commented upon. [Project of the Serbian Ministry of Education, Science and Technological Development, Grant no. 35035]
KEYWORDS
PAPER SUBMITTED: 2016-05-18
PAPER REVISED: 2016-06-21
PAPER ACCEPTED: 2016-07-04
PUBLISHED ONLINE: 2016-08-07
DOI REFERENCE: https://doi.org/10.2298/TSCI160518198P
CITATION EXPORT: view in browser or download as text file
THERMAL SCIENCE YEAR 2017, VOLUME 21, ISSUE Supplement 3, PAGES [S795 - S807]
REFERENCES
  1. Marvin, J. G., Coakley, T. J., Turbulence Modeling for Hypersonic Flows, Technical Memorandum No. 101079, Ames Research Center, Moffet Field, Cal., 1989
  2. Smits, J. A., et al., Current Status of Basic Research in Hypersonic Turbulence, 39th AIAA Fluid Dynamics Conference and Exhibit, Orlando, FL, 2009, paper 2009-151, pp. 1-32
  3. Roy J. C., Blottner G. F., Review and Assessment of Turbulence Models for Hypersonic Flows: 2D/Axisymmetric Cases, 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006, Reno, NV, AIAA 2006-713, pp.1-99.
  4. Savio E., Maciel G., Comparison of Several Turbulence Models as Applied to Hypersonic Flows in 2D - Part II, AASCIT Journal of Physics, 1 (2015), 4, pp. 275-287
  5. Roy J. C., Blottner G. F., Methodology for Turbulence Model Validation: Application to Hypersonic Flows, Journal of Spacecraft and Rockets, 40 (2003), 3, pp. 313-325
  6. Longo J. M. A., et al., The Challenge of Modeling High Speed Flows, Conference paper, 6th EUROSIM Congress on Modelling and Simulation, Ljubljana, Slovenia, 2007
  7. Liang W., Song F., Modeling Flow Transition in a Hypersonic Boundary Layer with Reynolds-Averaged Navier-Stokes Approach, Science in China Series G: Physics, Mechanics & Astronomy, 52 (2009), 5, pp. 768-774
  8. Tissera S., Assesment of High-Resolution Methods in Hypersonic Real-Gas Flows, Ph. D. thesis, Cranfield University, Cranfield, UK, 2010
  9. Wu M., Martin P. M., Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp, AIAA Journal, 45 (2007), 4, pp. 879-889
  10. Loginov S. M., Large-Eddy Simulation of Shock Wave/Turbulent Boundary Later Interaction, Ph. D. thesis, Technische Universitat Munchen, Munich, Germany, 2006
  11. ***, ANSYS FLUENT Theory Guide, ANSYS, Inc., Canonsburg, PA, 2015
  12. ***, ANSYS FLUENT User Guide, ANSYS, Inc., Canonsburg, PA, 2015
  13. Schulein E., et al., Documentation of Two-Dimensional Impinging Shock/Turbulent Boundary Layer Interaction Flow, Technical Report IB 223-96 A 49, German Aerospace Center (DLR), Gottingen, Germany, 1996
  14. Gray D. J., Summary Report on Aerodynamic Characteristics of Standard Models HB-1 and HB-2, Technical Report No. AEDC-TDR-64-137, Von Karman Dynamics Facility, 1964

© 2019 Society of Thermal Engineers of Serbia. Published by the Vinča Institute of Nuclear Sciences, Belgrade, Serbia. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution-NonCommercial-NoDerivs 4.0 International licence