The flow over a backward facing step is a classic problem in applied aerodynamics. Among many other applications, backward facing steps are often used for ignition and stabilization of the flame in a scramjet engine. In this study, the steady two-dimensional viscous supersonic turbulent flow over a backward facing step was calculated using FLUENT. The one-equation Spalart and Allmaras turbulence model was employed for the turbulent flow simulation. The free stream Mach number was 2. The simulated flow field is in good qualitative agreement with flow visualizations, pressure and temperature measurements and theoretical predictions. The boundary layer ahead of the step turns through the right angle over the corner. Then a separation occurs below the corner on the step wall. The numerical results indicate that the separation point is positioned on the step face, below the corner. The overexpansion at the corner is balanced by a lip-shock. This phenomenon was observed in experimental measurements, in flow visualizations and is also obtained in the present numerical calculation.
Skip Nav Destination
ASME 2004 International Mechanical Engineering Congress and Exposition
November 13–19, 2004
Anaheim, California, USA
Conference Sponsors:
- Fluids Engineering Division
ISBN:
0-7918-4709-8
PROCEEDINGS PAPER
Numerical Modeling of the Turbulent Supersonic Flow Over a Backward Facing Step
Valery Ponyavin,
Valery Ponyavin
University of Nevada at Las Vegas
Search for other works by this author on:
Yitung Chen,
Yitung Chen
University of Nevada at Las Vegas
Search for other works by this author on:
Darrell W. Pepper,
Darrell W. Pepper
University of Nevada at Las Vegas
Search for other works by this author on:
Hsuan-Tsung Hsieh
Hsuan-Tsung Hsieh
University of Nevada at Las Vegas
Search for other works by this author on:
Valery Ponyavin
University of Nevada at Las Vegas
Yitung Chen
University of Nevada at Las Vegas
Darrell W. Pepper
University of Nevada at Las Vegas
Hsuan-Tsung Hsieh
University of Nevada at Las Vegas
Paper No:
IMECE2004-59856, pp. 527-534; 8 pages
Published Online:
March 24, 2008
Citation
Ponyavin, V, Chen, Y, Pepper, DW, & Hsieh, H. "Numerical Modeling of the Turbulent Supersonic Flow Over a Backward Facing Step." Proceedings of the ASME 2004 International Mechanical Engineering Congress and Exposition. Fluids Engineering. Anaheim, California, USA. November 13–19, 2004. pp. 527-534. ASME. https://doi.org/10.1115/IMECE2004-59856
Download citation file:
8
Views
Related Proceedings Papers
Related Articles
Investigation on Turbulent Expansion-Corner Flow With Shock Impingement
J. Fluids Eng (March,2001)
Aerobreakup in Rarefied Supersonic Gas Flows
J. Fluids Eng (July,2004)
Related Chapters
Applications
Introduction to Finite Element, Boundary Element, and Meshless Methods: With Applications to Heat Transfer and Fluid Flow
Hybrid Parallel Programming on HPC Platform for 3D Scramjet Simulation
International Conference on Computer Technology and Development, 3rd (ICCTD 2011)
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)