supported by the National Natural Science Foundation of China(Grant Nos.10932005 and 11202115)
Competition of multiple Gortler modes in hypersonic boundary layer flows are investigated with the local and marching methods. The wall-layer mode (mode W) and the trapped-layer mode (mode T) both occur in the com...
supported by the National Natural Science Foundation of China(Grant Nos.10932005 and 11202115)
Nonlinear parabolized stability equations are employed in this work to investigate the nonlinear development of the G6rtler insta- bility up to the saturation stage. The perturbed boundary layer is highly inflectional...
supported by the GE Aviation under its University Strategic Alliance(USA) program;supported by the National Natural Science Foundation of China(Grant Nos.10932005 and 11272183)
The paper investigates the effect of a single circumferential groove casing treatment(CGCT) on a transonic compressor rotor numerically.In particular,the effect of the groove at different axial locations on the flow f...
supported by the National Natural Science Foundation of China (Grant Nos.10932005,10972120 and 11102098);the China Postdoctoral Science Foundation (Grant No.2011M500301)
Flow separation in a conical diffuser with large divergence angle (29.14°) and large area ratio (3.533) is eliminated by a novel passive flow control device called Karman-Vortex Generator (KVG). The effect of t...
supported by the National Natural Science Foundation of China (Grant Nos.10932005 and 50910222)
Direct numerical simulations are carried out to assess the potential drag reduction of compressible turbulent flow between isothermal walls.For the sake of achieving drag reduction,the flow is actively controlled by d...