An implicit essentially nonoscillatory method for the direct simulation of supersonic turbulent boundary layers

An implicit essentially nonoscillatory method for the direct simulation of supersonic turbulent boundary layers

Author(s):

Weirs, V. Gregory ( University of Minnesota and Army High Performance Computing Research Center )
Olejniczak, Debra J. ( University of Minnesota and Army High Performance Computing Research Center )
Candler, Graham V. ( University of Minnesota and Army High Performance Computing Research Center )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1998

Pub. Year:

1998

No.:

98-0129

Paper no.:

98-0129

Page(from):

1

Page(to):

11

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050859
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1998.01.12-1998.01.15
Note for article:	36th Aerospace Sciences Meeting & Exhibit, January 12-15, 1998/Reno, NV

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