| タイトル | Method of making counterrotating aircraft propeller blades |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080008730 |
| 著者（英） | Nelson, Joey L.; Elston, III, Sidney B.; Hemsworth, Martin C.; Tseng, Wu-Yang |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1990-11-20 |
| 言語 | eng |
| 内容記述 | An aircraft propeller blade is constructed by forming two shells of composite material laminates and bonding the two shells to a metallic spar with foam filler pieces interposed between the shells at desired locations. The blade is then balanced radially and chordwise. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | No Copyright |
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