| 翻訳と辞書 |
Hy-V
The Hy-V Scramjet Flight Experiment is a research project being led by the University of Virginia, the goal of which is to better understand dual-mode scramjet combustion by analyzing and comparing wind tunnel and flight data. The work is being conducted with industrial, academic and government collaborators.
==Overview==
The goal of the (Hy-V ) project is to conduct a flight experiment of a scramjet engine at Mach 5 using a sounding rocket. Currently the project is in its design and test phase and plans to launch a flight test in the future. In a dual-mode scramjet, combustion can either occur at subsonic or supersonic speeds, or a mixture of the two. The experiment will be performed at speed of Mach 5 because significant effects on mode transition occur at this speed. In this particular case, the mode transition will occur inside the scramjet when the vehicle's airspeed reaches Mach 5. Teams of students, both undergraduate and graduate, and faculty from the member universities of the (Virginia Space Grant Consortium ) are involved in the project and are collaborating with aerospace industry, NASA, and the Department of Defense.〔Goyne, CP, Cresci, D and Fetterhoff, TP, “Short Duration Propulsion Test and Evaluation (Hy-V) Program,” International Journal of Hypersonics, Vol 1, No 2, 2010, pp. 77-92〕
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
■ウィキペディアで「Hy-V」の詳細全文を読む
スポンサード リンク
| 翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|