[图书][B] Flow visualization: techniques and examples
AJ Smits - 2012 - books.google.com
This is the 2nd edition of the book, Flow Visualization: Techniques and Examples, which
was published by Imperial College Press in 2000. Many of the chapters have been revised …
was published by Imperial College Press in 2000. Many of the chapters have been revised …
Asymmetries in Nominally Symmetric Flows
OJH Williams, AJ Smits - Annual Review of Fluid Mechanics, 2024 - annualreviews.org
Many flows that are expected to be symmetric are actually observed to be asymmetric. The
appearance of asymmetry in the face of no particular cause is a widespread although …
appearance of asymmetry in the face of no particular cause is a widespread although …
Recent progress on the study of asymmetric vortex flow over slender bodies
XY Deng, W Tian, BF Ma, YK Wang - Acta Mechanica Sinica, 2008 - Springer
The investigations of forebody vortex flow and its flow control have great importance in both
academic field and engineering application areas. A large number of papers and many …
academic field and engineering application areas. A large number of papers and many …
Influence of nose perturbations on behaviors of asymmetric vortices over slender body
C Xuerui, D Xueying, W Yankui, L Peiqing… - Acta Mechanica Sinica, 2002 - Springer
The influence of nose perturbations on the behaviors of asymmetric vortices over a slender
body with a three-caliber ogive nose is studied in this paper. The tests of a nose-disturbed …
body with a three-caliber ogive nose is studied in this paper. The tests of a nose-disturbed …
Unsteady aerodynamic characteristics of slender body at extra-wide angle-of-attack range
F Wang, J Liu, H Qin, Y Song, L Chen, J Hu - Aerospace Science and …, 2021 - Elsevier
For complicated unsteady separated flow problem of slender body at extra-wide of angle of
attack range, delayed detached eddy simulation based on shear stress transport turbulence …
attack range, delayed detached eddy simulation based on shear stress transport turbulence …
A physical model of asymmetric vortices flow structure in regular state over slender body at high angle of attack
X Deng, G Wang, X Chen, Y Wang, P Liu… - Science in China Series E …, 2003 - Springer
In subcritical Reyolds number flow region, the repeatable and determinate asymmetric
vortices flow at regular state can be obtained by manually setting mini-perturbation on the …
vortices flow at regular state can be obtained by manually setting mini-perturbation on the …
Mechanism of side force generation and its alleviation over a slender body
P Kumar, JK Prasad - Journal of Spacecraft and Rockets, 2016 - arc.aiaa.org
Experiments and computational studies were made on a slender body having a slender ratio
of 16 at a freestream velocity of 17 m/s and Reynolds number of 2.9× 10 4 based on the …
of 16 at a freestream velocity of 17 m/s and Reynolds number of 2.9× 10 4 based on the …
Regimes identification of the viscous flow past an elliptic cylinder for Reynolds number up to 10000
In the present paper, the study of different regimes arising from the incompressible planar
viscous flow past an elliptical cylinder is presented. In order to highlight the effect of the …
viscous flow past an elliptical cylinder is presented. In order to highlight the effect of the …
Asymmetric vortices flow over slender body and its active control at high angle of attack
D Xueying, W Yankui - Acta Mechanica Sinica, 2004 - Springer
The studies of asymmetric vortices flow over slender body and its active control at high
angles of attack have significant importance for both academic field and engineering area …
angles of attack have significant importance for both academic field and engineering area …
Continuous control of asymmetric forebody vortices in a bi-stable state
Q Wang, K Cheng, Y Gu, Z Li - Physics of Fluids, 2018 - pubs.aip.org
Aiming at the problem of continuous control of asymmetric forebody vortices at a high angle
of attack in a bi-stable regime, a dual synthetic jet actuator embedded in an ogive forebody …
of attack in a bi-stable regime, a dual synthetic jet actuator embedded in an ogive forebody …