| タイトル | Large scale prop-fan structural design study. Volume 2: Preliminary design of SR-7 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900000728 |
| 著者（英） | Leishman, D. K.; Billman, L. C.; Turnberg, J. E.; Ladden, R. M.; Gruska, C. J. |
| 著者所属（英） | Hamilton Standard |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | In recent years, considerable attention has been directed toward improving aircraft fuel consumption. Studies have shown that the inherent efficiency advantage that turboprop propulsion systems have demonstrated at lower cruise speeds may now be extended to the higher speeds of today's turbofan and turbojet-powered aircraft. To achieve this goal, new propeller designs will require features such as thin, high speed airfoils and aerodynamic sweep, features currently found only in wing designs for high speed aircraft. This is Volume 2 of a 2 volume study to establish structural concepts for such advanced propeller blades, to define their structural properties, to identify any new design, analysis, or fabrication techniques which were required, and to determine the structural tradeoffs involved with several blade shapes selected primarily on the basis of aero/acoustic design considerations. The feasibility of fabricating and testing dynamically scaled models of these blades for aeroelastic testing was also established. The preliminary design of a blade suitable for flight use in a testbed advanced turboprop was conducted and is described. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 90N10044
NASA-CR-174993
NAS 1.26:174993
HSER-11518-VOL-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/140439 |
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