| タイトル | Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160005997 |
| 著者（英） | Li, Wu |
| 発行日 | 2015-06-22 |
| 言語 | eng |
| 内容記述 | This paper documents a process for analyzing whether a particular supersonic aircraft configuration layout and a given cruise condition are feasible to achieve a trimmed low-boom design. This process was motivated by the need to know whether a particular configuration at a given cruise condition could be reshaped to satisfy both low-boom and flight trim constraints. Without such a process, much effort could be wasted on shaping a configuration layout at a cruise condition that could never satisfy both low-boom and flight trim constraints simultaneously. The process helps to exclude infeasible configuration layouts with minimum effort and allows a designer to develop trimmed low-boom concepts more effectively. A notional low-boom supersonic demonstrator concept is used to illustrate the analysis/design process. |
| NASA分類 | Acoustics; Aerodynamics |
| レポートNO | NF1676L-19916 |
| 権利 | No Copyright |
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