Experimental and computational study on reduction of aerodynamic heating load by film cooling in hypersonic flows

Experimental and computational study on reduction of aerodynamic heating load by film cooling in hypersonic flows

Author(s):

Aso, S. ( Kyushu Univ., Japan )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1997

Pub. Year:

1997

No.:

97-0770

Paper no.:

97-0770

Page(from):

1

Page(to):

14

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050850
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	35th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1997.01.06-1997.01.10
Note for article:	35th Aerospace Sciences Meeting & Exhibit, January 6-10, 1997/Reno, NV

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