| タイトル | Interface concerns of ejector integration in V/STOL aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800001890 |
| 著者（英） | Lowry, R. B. |
| 著者所属（英） | Air Force Flight Dynamics Lab. |
| 発行日 | 1979-09-01 |
| 言語 | eng |
| 内容記述 | A number of areas which have in the past contributed to weight, complexity, and thrust losses in the ejector-powered V/STOL vehicle were identified. Most of these interfaces taken singly do not represent a severe compromise to the vehicle; however, the bottom line is that the sum of compromises and the subsequent effects on performance, flight operations and maintenance have rendered the ejector V/STOL aircraft unattractive. In addition to some of the unique ejector/aircraft integration problems, the vehicle by virtue of having a V/STOL capability, is compromised in other areas. To be successful and acceptable, the advantages must outweight the disadvantages and simplicity with minimum penalties must be the rule. It is concluded that more emphasis must be placed on the ejector/aircraft interface for the concept to be successful. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 80N10129 |
| 権利 | No Copyright |
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