Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps

Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps

Author(s):

N. Qin ( University of Sheffield, Sheffield, Great Britain )
S. Wong
A. Le Moigne

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-0057

Paper no.:

AIAA Paper 2007-57

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200701 [CD-ROM 2007 Disc 1]

Type:

Technical Paper

Details

TDL ID:	ZA00050739
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	45th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2007.01.08-2007.01.11

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