Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art

Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art

Author(s):

A. Paranjape ( Indian Institute of Technology, Bombay, Mumbai, India )
N. Sinha ( Indian Institute of Technology, Madras, Chennai, India )
N. Ananthkrishnan ( Zeus Numerix Pvt Ltd, IIT Bombay Campus, Mumbai, India )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-1051

Paper no.:

AIAA Paper 2007-1051

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200705 [CD-ROM 2007 Disc 5]

Type:

Technical Paper

Details

TDL ID:	ZA00049493
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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