Effects of Leading Edge Protuberances on Airfoil Performance
- Author(s):
- A. Levshin ( Worcester Polytechnic Institute, Worcester, MA )
- H. Johari
- C. Henoch ( Naval Undersea Warfare Center, Newport, RI )
- D. Custodio ( WPI, Worcester, MA )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Fluid Dynamics Conference
- Ser. no.:
- 2006
- Pub. Year:
- 2006
- No.:
- 2006-2868
- Paper no.:
- AIAA Paper 2006-2868
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200611 [CD-ROM 2006 Disc 11]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
A Transient Calorimeter Technique for Determining Regional Heat Transfer Coefficients in the Three-Temperature Flowfield at a Turbine Airfoil Leading Edge.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Highly turbulent mainstream effects on film cooling of a simulated airfoil leading edge
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
6
Technical Paper
Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Impact of Non-Uniform Leading Edge Coatings on the Aerodynamic Performance of Compressor Airfoils.
American Society of Mechanical Engineers |