Computations of Roll-Damping Stability Derivative for Body/Cruciform-Tail Configuration

Computations of Roll-Damping Stability Derivative for Body/Cruciform-Tail Configuration

Author(s):

Publication title:

A collection of technical papers : 20th AIAA Applied Aerodynamics Conference, St. Louis, Missouri, 24-27 June 2002

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-2721

Paper no.:

AIAA-2002-2721

Page(from):

75

Page(to):

82

Pages:

8

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475450 [1563475456]

Language:

English

Call no.:

A07400/022712

Type:

Technical Paper

Details

TDL ID:	ZA00001451
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	20th
Conf. info. (Venue):	St. Louis, Missouri
Conf. info. (Date):	2002.06.24-2002.06.27

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