A conceptual study of high speed rotorcraft
A conceptual study of high speed rotorcraft
dc.contributor.author | Tanabe, Y. | |
dc.contributor.author | Aoyama, T. | |
dc.contributor.author | Kobiki, N. | |
dc.contributor.author | Sugiura, M. | |
dc.contributor.author | Miyashita, R. | |
dc.contributor.author | Sunada, S. | |
dc.contributor.author | Kawachi, K. | |
dc.contributor.author | Nagao, M. | |
dc.date.accessioned | 2016-12-16T15:14:39Z | |
dc.date.available | 2016-12-16T15:14:39Z | |
dc.date.issued | 2014 | |
dc.description.abstract | A study group of future rotorcraft is formed in JAXA with participants from a wide spectra of organizations in Japan. Taking the helicopter market in Japan as a study case, four potential high speed rotorcraft (VTOL aircraft) missions are discussed. When a capability of hovering is required, compound helicopter is concluded as the most suitable design configuration. A simplified conceptual design process for a compound helicopter is described where a wing and propellers are added to a single rotor helicopter. A compound helicopter concept for high speed EMS (Emergency Medical Service) is proposed. The result of the conceptual design is compared with a conventional helicopter and the cost expense is illustrated. If also considering the cost to maintain a base hospital, a high speed rotorcraft with significant higher cost is acceptable which covers a much wider area providing effective first aid to critical patients | |
dc.identifier.other | 33-B-paper | |
dc.identifier.uri | http://hdl.handle.net/20.500.11881/3501 | |
dc.language.iso | en | |
dc.title | A conceptual study of high speed rotorcraft |
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