Subsonic Aerodynamic Fin-Folding Moments for the Tactical Tomahawk Missile Configuration

Author(s):

McGrath, B. ( Johns Hopkins University Applied Physics Laboratory, Laurel, MD )  

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

22nd

Pub. Year:

2004

No.:

2004-5193

Paper no.:

AIAA Paper 2004-5193

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200414 [CD-ROM 2004 Disc 14]

Type:

Technical Paper