Effects of Shock and Boundary-Layer Control Techniques on Transonic Flows about Airfoils

Effects of Shock and Boundary-Layer Control Techniques on Transonic Flows about Airfoils

Author(s):

Dima, C. ( C.I.R.A. - Centro Italiano Ricerche Aerospaziali )
deMatteis, P.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-0517

Paper no.:

00-0517

Page(from):

1

Page(to):

6

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050874
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospaces Science Meeting and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2000.01.10-2000.01.13
Note for article:	38th Aerospace Sciences Meeting & Exhibit 10-13 January 2000 / Reno, NV

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