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Investigation of a nearly isentropic mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.2

机译：研究几乎等熵的混合压缩轴对称入口系统，马赫数为0.6至3.2

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摘要

Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio, pressure recovery and pressure distortion

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作者
Smeltzer, D. B.; Sorensen, N. E.;
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年度 1968
页码 1-152
总页数 152
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
INLET PRESSURE; MASS FLOW; PRESSURE RECOVERY; SUPERSONIC DIFFUSERS; ANGLE OF ATTACK; GRAPHS (CHARTS); PRESSURE DISTRIBUTION; SUPERSONIC WIND TUNNELS; TABLES (DATA);

机译：进口压力;质量流量;压力恢复;超音速扩散器;攻击角度;图表（图表）;压力分布;超级风洞;表（数据）;

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专利

1. Forced Oscillations in a Mixed-Compression Inlet at Mach 3.5 for Pulse Detonation Engine Systems [J] . Venkata Nori, Nelson Lerma, Jonas Gustavsson, Journal of Fluids Engineering: Transactions of the ASME . 2006,第3期

机译：脉冲爆震发动机系统的混合压缩进气中的强迫振荡（马赫数为3.5）
2. Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression [J] . Galkin V. M., Vnuchkov D. A., Zvegintsev V. I. Journal of Applied Mechanics and Technical Physics . 2015,第5期

机译：等轴压缩轴对称隧道进气口的气动设计
3. The low Mach number limit for the isentropic Euler system with axisymmetric initial data [J] . Hmidi T. Journal of the Institute of Mathematics of Jussieu: JIMJ . 2013,第2期

机译：具有轴对称初始数据的等熵Euler系统的马赫数下限
4. Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed [C] . T. Conners, J. Merret, D. Howe, AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2007

机译：设计速度为1.97马赫的轴对称各向同性松弛外部压缩入口的风洞测试
5. Numerical Investigation of Magnetically Driven Isentropic Compression of Solid Aluminum Cylinders with a Semi-Analytical Code. [D] . Largent, Billy T. 2017

机译：用半解析代码对固态铝缸的电磁等熵压缩进行数值研究。
6. Luminescent Measurement Systems for the Investigation of a Scramjet Inlet-Isolator [O] . Azam Che Idris, Mohd Rashdan Saad, Hossein Zare-Behtash, 2014

机译：用于研究超燃冲压发动机进气口隔离器的发光测量系统
7. CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet [O] . Conners Timothy R., Tacina Kathleen M., Hirt Stefanie M., 2008

机译：轴对称各向同性松弛压缩入口的CFD结果
8. Investigation of a Nearly Isentropic Mixed Compression Axisymmetric Inlet System at Mach Numbers 0.6 to 3.2 [R] . Smeltzer, D. B., Sorensen, N. E. 1968

机译：近似等熵混合压缩轴对称进气系统的研究，马赫数为0.6至3.2

Investigation of a nearly isentropic mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.2

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