| タイトル | Preliminary design of a supersonic Short Takeoff and Vertical Landing (STOVL) fighter aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900014078 |
| 著者（英） | Ross, Tweed, III; Henderson, Dean; Bellmard, Larry; Jacobs, Tavis; Gomer, Charlie; Peterson, Eric; Lawson, Todd; Cox, Brian; Borchers, Paul |
| 著者所属（英） | Kansas Univ. |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | The preliminary design study of a supersonic Short Takeoff and Vertical Landing (STOVL) fighter is presented. A brief historical survey of powered lift vehicles was presented, followed by a technology assessment of the latest supersonic STOVL engine cycles under consideration by industry and government in the U.S. and UK. A survey of operational fighter/attack aircraft and the modern battlefield scenario were completed to develop, respectively, the performance requirements and mission profiles for the study. Three configurations were initially investigated with the following engine cycles: a hybrid fan vectored thrust cycle, a lift+lift/cruise cycle, and a mixed flow vectored thrust cycle. The lift+lift/cruise aircraft configuration was selected for detailed design work which consisted of: (1) a material selection and structural layout, including engine removal considerations, (2) an aircraft systems layout, (3) a weapons integration model showing the internal weapons bay mechanism, (4) inlet and nozzle integration, (5) an aircraft suckdown prediction, (6) an aircraft stability and control analysis, including a takeoff, hover, and transition control analysis, (7) a performance and mission capability study, and (8) a life cycle cost analysis. A supersonic fighter aircraft with STOVL capability with the lift+lift/cruise engine cycle seems a viable option for the next generation fighter. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 90N23394
NASA-CR-186670
NAS 1.26:186670 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/137647 |
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