Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow

Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow

Author(s):

Publication title:

A collection of technical papers : 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, 4-6 September 2002

Title of ser.:

AIAA Paper : Symposium on Multidisciplinary Analysis and Optimization

Ser. no.:

2002

Pub. Year:

2002

Vol.:

v. 2

No.:

2002-5547

Paper no.:

AIAA-2002-5547

Page(from):

1326

Page(to):

1335

Pages:

10

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475504 [1563475502]

Language:

English

Call no.:

A07400/025400 (v.2)

Type:

Technical Paper

Details

TDL ID:	ZA00001459
Series ID:	PA00000159
Conf. info. (Name):	AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Conf. info. (Number):	9th
Conf. info. (Venue):	Atlanta, Georgia
Conf. info. (Date):	2002.09.04-2002.09.06

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