Aerodynamic Characteristics of Fan-Jet STOL Aircraft
| Autor: | INUMARU, Norio, TAKAHASHI, Hitoshi, HIROSUE, Kenichi, TODA, Nobuhiro, KUWANO, Naoaki |
|---|---|
| Jazyk: | japonština |
| Rok vydání: | 1983 |
| Zdroj: | 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-790. 790:99 |
| ISSN: | 0389-4010 |
| Popis: | Research on Fan-Jet STOL aircraft was initiated by NAL in 1975 as a wind-tunnel-based program aimed at the design study of experimental STOL aircraft. Aerodynamic characteristics of the Augmentor Wing type model and the Upper Surface Blowing type models are examined by a series of wind-tunnel tests. Three-component longitudinal data of each model are presented. Six-component lateral data of a USB type model are also presented with four engines operating and with one engine out. The general aerodynamic trends of Powered-Lift systems are discussed through comparison with existing data. Discussions concerning the test-techniques are also included. The research was concluded in 1979, making direct contributions to the basic design of NAL Quiet STOL Experimental Aircraft. 資料番号: NALTR0790000 レポート番号: NAL TR-790 |
| Databáze: | OpenAIRE |
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