Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility-Reference-Cited by-同舟云学术

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Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility

Published:2019-03-01 Issue:2 Volume:12 Page:461-468
ISSN:1735-3572
Container-title:Journal of Applied Fluid Mechanics
language:en
Short-container-title:JAFM

Author:

Saiprakash M.,Senthil Kumar C.,Sunil G. K.,Rampratap S. P.,Shanmugam V.,Balu G., , , , , ,

Publisher

Academic World Research

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Supersonic Flow over Elliptic Cone with Different Ellipticity Ratio;Journal of Applied Fluid Mechanics;2023-12-01

2. An Investigation of Axisymmetric Glass Blown Mach 2 Nozzle for Flow and Surface Optical Diagnostics;AIAA Scitech 2021 Forum;2021-01-04

3. On the Application of Endoscopic Background-Oriented Schlieren Technique for Near-Field Investigation of Density Field;Journal of Applied Fluid Mechanics;2020-03-01

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