Prediction of the Nonlinear Aerodynamic Characteristics of Tandem-Control and Rolling-Tail Missiles

Prediction of the Nonlinear Aerodynamic Characteristics of Tandem-Control and Rolling-Tail Missiles

Author(s):

Publication title:

A collection of technical papers, AIAA Atmospheric Flight Mechanics Conference, Monterey, California, 5-8 August 2002

Title of ser.:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

Ser. no.:

2002

Pub. Year:

2002

Vol.:

v. 1

No.:

2002-4511

Paper no.:

AIAA-2002-4511

Page(from):

454

Page(to):

464

Pages:

11

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475474 [1563475472]

Language:

English

Call no.:

A07400/024400 (v.1)

Type:

Technical Paper

Details

TDL ID:	ZA00001453
Series ID:	PA00000162
Conf. info. (Name):	AIAA Atmospheric Flight Mechanics Conference
Conf. info. (Number):	2002
Conf. info. (Venue):	Monterey, California
Conf. info. (Date):	2002.08.05-2002.08.08

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