Blank Cover Image

THE SIMULATION OF THREE-DIMENSIONAL VISCOUS SUPERSONIC FLOW PAST BLUNT BODIES WITH A HYBRID IMPLICIT/EXPLICIT FINITE-DIFFERENCE METHOD

Author(s):
RIEDELBAUCH, S. et al. ( DFVLR, GOETTINGEN, WEST GER. )  
Publication title:
NASA Technical Reports(N88-)
Pub. Year:
1987
Issue:
DFVLR-FB-87-32
Paper no.:
N88-15765
Page(from):
1
Page(to):
62
Pages:
62
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

Similar Items:

RIEDELBAUCH, S.

National Aeronautics and Space Administration

Asif, M., Zahir, S., Kamran, N., Khan, M.

American Institute of Aeronautics and Astronautics

Khalid,M., Chen,S., Xu,H.

American Institute of Aeronautics and Astronautics

Weber, K. F., Delaney, R. A.

The American Society of Mechanical Engineers

He, H., Yu, S.-T.J.

American Institute of Aeronautics and Astronautics

Li, J., Huang, S., Jiang, S., Li, F.

American Institute of Aeronautics and Astronautics

Agarwal, Ramesh K., Augustinus, Justin

American Institute of Aeronautics and Astronautics

H. Kim, S. Aradag, D. Knight

American Institute of Aeronautics and Astronautics

Guo,K.L., Liaw,G.S.

American Institute of Aeronautics and Astronautics

Agarwal, Ramesh K., Augustinus, Justin

American Institute of Aeronautics and Astronautics

JUN, L.

National Aeronautics and Space Administration

1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12