Aerodynamic Analysis of a Spinning Missile with Dithering Canards Using a High Order Unstructured Grid Scheme

Aerodynamic Analysis of a Spinning Missile with Dithering Canards Using a High Order Unstructured Grid Scheme

Author(s):

C. Sheng ( Mississippi State University, MS )
X. Wang

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-1090

Paper no.:

AIAA Paper 2009-1090

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200901

Type:

Technical Paper

Details

TDL ID:	ZA00052180
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
Conf. info. (Number):	47th
Conf. info. (Venue):	Orlando, Florida
Conf. info. (Date):	2009.01.05-2009.01.08
Note for article:	47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 5-8 January 2009, Orlando, Florida

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