INVESTIGATION OF ARTIFICIALLY BLUNTED LEADING EDGE GEOMETRIES WITH CURVED CHANNELS FOR HIGH SPEED DRAG REDUCTION

INVESTIGATION OF ARTIFICIALLY BLUNTED LEADING EDGE GEOMETRIES WITH CURVED CHANNELS FOR HIGH SPEED DRAG REDUCTION

Author(s):

Gupta, Anurag ( National Institute for Aviation Research )
Ruffin, Stephen M.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-0901

Paper no.:

00-0901

Page(from):

1

Page(to):

12

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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