Experiment and prediction of a cavity type separated flow

1996 ◽  
Vol 56 (4) ◽  
pp. 299-311 ◽  
Author(s):  
MD. Mujibur Rahman ◽  
J. A. Naser
Keyword(s):  
Separated Flow

VELOCITY AND TEMPERATURE DISTRIBUTIONS AT THE TURBULENT SEPARATED FLOW BEHIND BACKSTEP IN THE CHANNEL

1994 ◽  
Author(s):  
P. L. Komarov ◽  
V. V. Kulish ◽  
Anatoly F. Polyakov ◽  
Aleksey Yur'evich Varaksin
Keyword(s):  
Separated Flow ◽  
Temperature Distributions ◽  
Turbulent Separated Flow

Three-dimensional separated flow adjacent to backward-facing step

2002 ◽  
Author(s):  
Bassem F. Armaly ◽  
Jianhu Nie ◽  
An Li
Keyword(s):  
Three Dimensional ◽  
Separated Flow ◽  
Backward Facing Step

FORMATION OF STREAMWISE VORTICES BEHIND THE LINE OF SUPERSONIC SEPARATED FLOW REATTACHMENT AT A COMPRESSION CORNER

2016 ◽  
Vol 47 (3) ◽  
pp. 267-281 ◽  
Author(s):  
Valeriy Ivanovich Zapryagaev ◽  
Ivan Nikolayevich Kavun
Keyword(s):  
Separated Flow ◽  
Streamwise Vortices ◽  
Compression Corner ◽  
Flow Reattachment

Experimental Study of Flow Control Over a Standard Road Vehicle Using Plasma Actuator

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi
Keyword(s):  
Flow Control ◽  
Pressure Distribution ◽  
Drag Force ◽  
Separated Flow ◽  
Plasma Actuator ◽  
Road Vehicle ◽  
Slant Angle ◽  
Total Drag ◽  
Slant Surface ◽  
Ahmed Body

AbstractAhmed Body is a standard and simplified shape of a road vehicle that's rear part has an important role in flow structure and it's drag force. In this paper flow control around the Ahmed body with the rear slant angle of 25° studied by using the plasma actuator system situated in middle of the rear slant surface. Experiments conducted in a wind tunnel in two free stream velocities of U = 10m/s and U = 20m/s using steady and unsteady excitations. Pressure distribution and total drag force were measured and smoke flow visualization carried out in this study. The results showed that at U = 10m/s using plasma actuator suppress the separated flow over the rear slant slightly and be effective on pressure distribution. Also, total drag force reduces in steady and unsteady excitations for 3.65% and 2.44%, respectively. At U = 20m/s, using plasma actuator had no serious effect on the pressure distribution and total drag force.

High-Order Delayed Detached Eddy Simulation of Separated Flow with Self-Adaptive Dissipation

2020 ◽  
pp. 1-12
Author(s):  
Li Hao ◽  
Liu Wei ◽  
Wang Shengye ◽  
Wang Guangxue
Keyword(s):  
Separated Flow ◽  
High Order ◽  
Detached Eddy Simulation ◽  
Eddy Simulation ◽  
Delayed Detached Eddy Simulation ◽  
Self Adaptive

Control of separated flow behind a cylinder using discrete suction

AIAA Journal ◽  
2001 ◽  
Vol 39 ◽  
pp. 355-357
Author(s):  
T. Terry Ng
Keyword(s):  
Separated Flow
Sign in / Sign up

Export Citation Format

Share Document