首页> 美国政府科技报告 >Shock shapes and pressure distributions for large angle pointed cones in helium at Mach numbers of 8 and 20

【24h】

Shock shapes and pressure distributions for large angle pointed cones in helium at Mach numbers of 8 and 20

机译：氦气中大角度尖锥的冲击形状和压力分布，马赫数为8和20

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Shock shape and surface pressure measurements on hypersonic pointed cones in helium

著录项

作者
Inouye, M.; Stewart, D. A.;
展开▼
作者单位

展开▼
年度 1969
页码 1-22
总页数 22
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CONICAL BODIES; HELIUM; HYPERSONIC SHOCK; PRESSURE MEASUREMENT; PRESSURE DISTRIBUTION; SHOCK WAVE PROFILES; SURFACE PROPERTIES;

机译：圆锥体;氦;超级冲击;压力测量;压力分布;冲击波轮廓;表面特性;

相似文献

外文文献
中文文献
专利

1. Self-Generated Magnetic and Electric Fields at a Mach-6 Shock Front in a Low Density Helium Gas by Dual-Angle Proton Radiography [J] . Hua R., Kim J., Sherlock M., Physical review letters . 2019,第21期

机译：通过双角度质子造影，Mach-6在Mach-6处的自成磁场和电场在低密度氦气中冲击前部
2. Numerical Study of Flow Angles and Mach Number Measurement Using the Surface Pressure of a Supersonic Aircraft with Nose Cone [J] . Katsuyoshi Fukiba, Nobuyuki Tsuboi, Hiroaki Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2012,第2期

机译：超音速机鼻锥面流角和马赫数测量的数值研究。
3. Pressure Distribution & Calculation of Pressure Cone Angle [J] . Dave Archer Fastener technology international . 2010,第2期

机译：压力分布与压力锥角计算
4. Boundary-layer Separation Detection for a Cone at High Angle of Attack in Mach 4.5 Flow with Pressure-Sensitive Paint [C] . Carson L. Running, Michael J. Thompson, Thomas J. Juliano, AIAA Fluid Dynamics Conference;AIAA Aviation Forum . 2017

机译：压力敏感涂料在4.5马赫流动中高攻角锥的边界层分离检测
5. Parametric Study of a 7° Half-angle Cone with Highly-swept Fins at Mach 6 [D] . Turbeville, Franklin Drew. 2018

机译：在马赫6中具有高扫翅片的7°半角锥的参数研究
6. Penetration Characteristics of Air Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow [O] . Erinc Erdem, Konstantinos Kontis, Selvaraj Saravanan 2014

机译：空气二氧化碳和氦气横向声速射流在5马赫错流中的渗透特性
7. Numerical Study of Flow Angles and Mach Number Measurement Using the Surface Pressure of a Supersonic Aircraft with Nose Cone [O] . Katsuyoshi FUKIBA, Nobuyuki TSUBOI, Hiroaki KOBAYASHI 2012

机译：利用鼻锥形飞机表面压力的流动角度和马赫数测量的数值研究
8. Shock Shapes and Pressure Distributions for Large Angle Pointed Cones in Helium at Mach Numbers of 8 and 20 [R] . Inouye, M., Stewart, D. A. 1969

机译：马赫数为8和20的氦中大角度尖锥的冲击形状和压力分布

Shock shapes and pressure distributions for large angle pointed cones in helium at Mach numbers of 8 and 20

摘要

著录项

相似文献

相关主题

期刊订阅