Shock Wave

EDWARD H. PHILLIPS

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Shock Wave

机译：激波

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The world's first supersonic business jet could be flying by 2013, but proponents will have to overcome significant regulatory, industrial and environmental challenges to make that flight a reality. The chief roadblock to SSB J operations in the U.S. is regulatory, not technical. The FAA prohibits supersonic flight over land for commercial and private jets, and unless that rule can be eliminated or modified the future looks uncertain for would-be supersonic jet manufacturers. The primary reason is sonic boom, or aerodynamic overpressure, that occurs when an aircraft exceeds the speed of sound. Numerous solutions have been proposed and test-rned that would significantly reduce this phenomenon, but none of these would eliminate it altogether.

机译：世界上第一架超音速公务机可能会在2013年开始飞行，但支持者必须克服重大的监管，工业和环境挑战，才能实现这一飞行。在美国进行SSB J运营的主要障碍是法规，而不是技术。 FAA禁止超音速飞机用于民用和私人飞机的飞行，除非可以取消或修改该规则，否则对于未来的超音速飞机制造商来说，前途未卜。主要原因是当飞机超过声速时发生的音爆或空气动力学过压。已经提出并测试了许多解决方案，这些解决方案将大大减少这种现象，但是没有一个能够完全消除它。

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《Aviation Week & Space Technology》 |2007年第14期|50-52|共3页
作者
EDWARD H. PHILLIPS;
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收录信息美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
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1. Numerical Study of Shock Wave Attenuation in Two-Dimensional Ducts Using Solid Obstacles: How to Utilize Shock Focusing Techniques to Attenuate Shock Waves [J] . Hossein Zare-Behtash, Qian Wan, Veronica Eliasson Aerospace . 2015,第2期

机译：利用固体障碍物对二维风管中的冲击波衰减进行数值研究：如何利用冲击聚焦技术来衰减冲击波
2. Coronal Shock Waves, EUV Waves, and Their Relation to CMEs. III. Shock-Associated CME/EUV Wave in an Event with a Two-Component EUV Transient [J] . V. V. Grechnev, A. N. Afanasyev, A. M. Uralov, Solar Physics . 2011,第2期

机译：冠状冲击波，EUV波及其与CME的关系。三，具有两分量EUV瞬态的事件中与冲击相关的CME / EUV波
3. Coronal Shock Waves, EUV Waves, and Their Relation to CMEs. III. Shock-Associated CME/EUV Wave in an Event with a Two-Component EUV Transient [J] . Grechnev V.V., Afanasyev A.N., Uralov A.M., Solar physics . 2011,第2期

机译：冠状冲击波，EUV波及其与CME的关系。三，具有两分量EUV瞬变的事件中与冲击相关的CME / EUV波
4. ADMISSIBLE SHOCK WAVES AND SHOCK-INDUCED PHASE TRANSITION IN A VAN DER WAALS FLUID (PART II - RANKINE-HUGONIOT CONDITIONS AND SHOCK ADMISSIBILITY) [C] . T. RUGGERI, A. MENTRELLI, M. SUGIYAMA Conference on Waves and Stability in Continuous Media . 2010

机译：van der Waals流体中可接受的冲击波和震动诱导的相变（第二部分 - 兰氏蛋白 - Hugoniot条件和休克可容许性）
5. SHOCK WAVE DYNAMICS: (1) OSCILLATORY SHOCK WAVE MOTION PRODUCED BY A STRONG EXPLOSION AND A DRIVING PISTON IN A SPHERICALLY SYMMETRIC NONUNIFORM MEDIUM, (2) THE ADVANCE OF A BLAST WAVE INTO AN EXPONENTIALLY DECREASING DENSITY FIELD [D] . MOH, TZU-CHUNG -1

机译：冲击波动力学：（1）在球对称非均匀介质中强爆炸和推动活塞产生的振荡性冲击波运动；（2）爆炸波进入密度场成指数级下降的过程
6. Using 300 Pretreatment Shock Waves in a Voltage Ramping Protocol Can Significantly Reduce Tissue Injury During Extracorporeal Shock Wave Lithotripsy [O] . Bret A. Connors, Andrew P. Evan, Rajash K. Handa, -1

机译：在电压提升协议中使用300个预处理冲击波可以显着减少体外冲击波碎石术中的组织损伤
7. Trends in the development of detonation engines for high-speed aerospace aircrafts and the problem of triple configurations of shock waves. Part II - Research of counterpropagating shock waves and triple shock wave configurations [O] . P.V. Bulat, P.V. Denissenko 2016

机译：高速航空航天飞机爆轰发动机发展的趋势及冲击波三重配置问题。第二部分 - 对逆产冲击波和三重冲击波配置的研究
8. AN INTEGRAL SOLUTION TO THE FLAT-PLATE LAMINAR BOUNDARY-LAYER FLOW EXISTING INSIDE AND AFTER EXPANSION WAVES AND AFTER SHOCK WAVES MOVING INTO QUIESCENT FLUID WITH PARTICULAR APPLICATION TO THE COMPLETE SHOCK-TUBE FLOW [R] . Robert L. Trimpi, Nathaniel B. Cohen 1957

机译：膨胀波内部和冲击波后的平板层状边界层流动的积分解决方案，特别适用于完全冲击管流动的静态流体

Shock Wave

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