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Influence on Aerodynamic Performance of a Compound Helicopter by Wing Incidence Angle
- Source :
- 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences. 67(3):93(27)-101(35)
- Publication Year :
- 2019
- Publisher :
- 日本航空宇宙学会, 2019.
-
Abstract
- 形態: 図版あり<br />Physical characteristics: Original contains illustrations<br />資料番号: PA2020043000
- Subjects :
- Aerodynamic Drag
Rotor/Wing Interaction
CFD Simulation
Compound Helicopter
Subjects
Details
- Language :
- Japanese
- ISSN :
- 13446460
- Volume :
- 67
- Issue :
- 3
- Database :
- OpenAIRE
- Journal :
- 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
- Accession number :
- edsair.jairo.........fec8ace4f2f73654e30a4f32267f0b83