Wind Tunnel Measurements of the E-8C Modeled With and Without Winglets
- Author(s):
- M. Reeder ( Air Force Institute of Technology, Wright-Patterson AFB, OH )
- W. Allen
- J. Phillips ( U.S. Air Force , Wright-Patterson AFB, OH )
- R. Dimmick ( Northrop Grumman Integrated Systems, Melbourne, FL )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : U.S. Air Force T&E Days
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-1633
- Paper no.:
- AIAA Paper 2007-1633
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200706 [CD-ROM 2007 Disc 6]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Plans and Status of Wind-Tunnel Testing Employing an Aeroservoelastic Semispan Model
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Dynamic Response Tests of Inertial and Optical Wind-Tunnel Model Attitude Measurement Devices
National Aeronautics and Space Adminstration |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Wind Tunnel Study of Interference Effects Relating to Aft Supersonic Ejection of a Store
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
11
Technical Paper
Pressure Measurements Onboard a Small-Scale Rotating wind Tunnel Model for Jet/Fin Interaction.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |