| タイトル | High-Lift Propeller System Configuration Selection for NASA's SCEPTOR Distributed Electric Propulsion Flight Demonstrator |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160010105 |
| 著者（英） | Borer, Nicholas K.; Patterson, Michael D.; Derlaga, Joseph M. |
| 発行日 | 2016-06-13 |
| 言語 | eng |
| 内容記述 | Although the primary function of propellers is typically to produce thrust, aircraft equipped with distributed electric propulsion (DEP) may utilize propellers whose main purpose is to act as a form of high-lift device. These \high-lift propellers" can be placed upstream of wing such that, when the higher-velocity ow in the propellers' slipstreams interacts with the wing, the lift is increased. This technique is a main design feature of a new NASA advanced design project called Scalable Convergent Electric Propulsion Technology Operations Research (SCEPTOR). The goal of the SCEPTOR project is design, build, and y a DEP aircraft to demonstrate that such an aircraft can be much more ecient than conventional designs. This paper provides details into the high-lift propeller system con guration selection for the SCEPTOR ight demonstrator. The methods used in the high-lift propeller system conceptual design and the tradeo s considered in selecting the number of propellers are discussed. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NF1676L-22853 |
| 権利 | No Copyright |
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