|
|||||
|
|
| 一种负升力超高声速临近空间突击飞行概念 | |
| 引用本文： | 闫野. 一种负升力超高声速临近空间突击飞行概念[J]. 飞行力学, 2009, 27(1) |
| 作者姓名： | 闫野 |
| 作者单位： | 国防科技大学,航天与材料工程学院,湖南,长沙,410073 |
| 基金项目： | 国家高技术研究发展计划(863计划) |
| 摘 要： | 提出一种飞行高度70 km以上的超高速临近空间飞行概念,旨在通过火箭发动机克服大气阻力作用,通过负升力达到"增加"地球引力常数的等效效果,实现高于地球环绕速度的突击飞行,具有速度快、航程远的特点.分析了等高度巡航过程的受力情况,对气动参数选取、能量需求等问题进行了分析,给出了这类飞行器可能运行的空间区域.分析表明,该飞行方式可以实现在40 min内全球到达. |
| 关 键 词： | 临近空间 负升力 超高速飞行 |
Supersonic Velocity Onslaught Flight Concept with Subtractive Lift in Near Space |
|
| YAN Ye. Supersonic Velocity Onslaught Flight Concept with Subtractive Lift in Near Space[J]. Flight Dynamics, 2009, 27(1) | |
| Authors: | YAN Ye |
| Affiliation: | College of Aerospace and Material Engineering;National University ofDefense Technology;Changsha 410073;China |
| Abstract: | A concept of supersonic velocity craft in near space was presented,which flies at a height of over 70 kilometers.This craft conquered the atmosphere resistance with the thrust provided by the rocket engine and enhanced the gravity acceleration constant with the pneumatic subtractive lift to reach the onslaught flight at a velocity above the escape speed.This mode of flight possessed of the characteristics of high speed and long voyage.Some dynamics issues were discussed,such as pneumatic parameters selectio... |
| Keywords: | near space subtractive lift supersonic velocity flight |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |