Rolling moment characteristics at high alpha on several planforms of cranked arrow wing configuration
- Author(s):
- Kwak, Dong-Youn ( Japan Aerospace Exploration Agency, Mitaka, Tokyo, 181-0015, Japan )
- Hirai, Ketaro ( University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan )
- Rinoie, Kenichi ( University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan )
- Kato, Hiroyuki ( Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2009
- Pub. Year:
- 2009
- No.:
- 2009-3937
- Paper no.:
- AIAA Paper 2009-3937
- Pages:
- 9
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200907
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Roll Characteristics of an SST Configurations with Leading-Edge Flaps at High Alpha
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Aerodynamic Characteristics of Rolled SST Configuraton with LE and TE Flaps at High Angles of Attack
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
4
Technical Paper
Wall Interference Induced Rolling Moment Coefficient Correction For Realistic Wing Planforms
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
5
Technical Paper
Experimental Studies of Vortex Flaps and Vortex Plates Part 2 1.15 m Span 60○ Delta Wing
National Aeronautics and Space Adminstration |
11
Technical Paper
Analysis of Flows over a SST Wing-Body Configuration at Low Speed and High Angles of Attack
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Comparison of Rolling Moment Characteristics During Roll Oscillations for a Low and a High Aspect Ratio Configuration
American Institute of Aeronautics and Astronautics |
12
Technical Paper
AERODYNAMIC CHARACTERISTICS OF A HIGH-WING TRANSPORT CONFIGURATION WITH A OVER-THE-WING NACELLE-PYLON ARRANGEMENT
National Aeronautics and Space Administration |