Journal article

Numerical investigation of transitional supersonic base flows with flow control

J Sivasubramanian, RD Sandberg, DA Von Terzi, HF Fasel

Journal of Spacecraft and Rockets | American Institute of Aeronautics and Astronautics | Published : 2007


Drag reduction by means of flow control is investigated for supersonic base flows at M = 2.46 using direct numerical simulations and the flow simulation methodology. The objective of the present work is to understand the evolution of coherent structures in the flow and how flow control techniques can modify these structures. For such investigations, simulation methods that capture the dynamics of the large turbulent structures are required. Direct numerical simulations are performed for transitional base flows at ReD = 30,000. Because of the drastically increased computational cost of direct numerical simulations at higher Reynolds numbers, a hybrid methodology (flow simulation methodology) ..

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University of Melbourne Researchers