Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges, part II: receptivity to sound

Author(s):

Zhong, Xiaolin ( University of California, Los Angeles )  

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1997

Pub. Year:

1997

No.:

97-0756

Paper no.:

97-0756

Page(from):

1

Page(to):

19

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper