Three-dimensional calculation of transonic viscous flows by an implicit method

AIAA Journal ◽  
1985 ◽  
Vol 23 (11) ◽  
pp. 1670-1678 ◽  
Author(s):  
H. Hollanders ◽  
A. Lerat ◽  
R. Peyret

1995 ◽  
Vol 9 (6) ◽  
pp. 671-695 ◽  
Author(s):  
D. Mateescu ◽  
T. Pottier ◽  
L. Perotin ◽  
S. Granger


2000 ◽  
Author(s):  
P. Morgan ◽  
M. Visbal ◽  
P. Sadayappan




2007 ◽  
Vol 111 (1125) ◽  
pp. 699-704 ◽  
Author(s):  
G. Zhu ◽  
P. W. Bearman ◽  
J. M. R. Graham

AbstractThe present paper continues the work of Zhuet al. The closed-form expressions for the evaluation of forces on a body in compressible, viscous and rotational flow derived in the previous paper have been extended to different forms. The expressions require only a knowledge of the velocity field (and its derivatives) in a finite and arbitrarily chosen region enclosing the body. The equations are implemented on three-dimensional inviscid flows over wings and wing/body combinations. Further implementation on three-dimensional viscous flows over wings has also been investigated.







Sign in / Sign up

Export Citation Format

Share Document