An Experimental and CFD Investigation of a Supersonic Nonisobaric Jet Exhausting From a Beveled Nozzle

2014 ◽  
Vol 9 (2) ◽  
pp. 75-83
Author(s):  
Valeriy Zapryagaev ◽  
Ivan Kavun ◽  
Sergey Kundasev

The aim of the investigation is to understand the shock-wave structure of the supersonic jet exhausting from a beveled nozzle. Results of investigation are presented as cross section Pitotpressure fields. This data can be used for verification of CFD results. The experiment was complemented by numerical simulation with using of the program packet ANSYS Fluent. The satisfactory qualitative agreement was obtained

Fluids ◽  
2021 ◽  
Vol 6 (9) ◽  
pp. 305
Author(s):  
Mikhail V. Chernyshov ◽  
Karina E. Savelova ◽  
Anna S. Kapralova

In this study, we obtain the comparative analysis of methods of quick approximate analytical prediction of Mach shock height in planar steady supersonic flows (for example, in supersonic jet flow and in narrowing channel between two wedges), that are developed since the 1980s and being actively modernized now. A new analytical model based on flow averaging downstream curved Mach shock is proposed, which seems more accurate than preceding models, comparing with numerical and experimental data.


2007 ◽  
Vol 19 (6) ◽  
pp. 068102 ◽  
Author(s):  
Tatiana G. Elizarova ◽  
Anton A. Khokhlov ◽  
Salvador Montero

2009 ◽  
Vol 26 (1) ◽  
pp. 1-8
Author(s):  
Tsuyoshi Yasunobu ◽  
Yumiko Otobe ◽  
Hideo Kashimura ◽  
Shigeru Matsuo ◽  
Toshiaki Setoguchi ◽  
...  

Aerospace ◽  
2018 ◽  
Vol 5 (2) ◽  
pp. 60 ◽  
Author(s):  
Valery Zapryagaev ◽  
Nikolay Kiselev ◽  
Dmitry Gubanov

1998 ◽  
Vol 64 (619) ◽  
pp. 732-739
Author(s):  
Tomoyoshi KOBAYASI ◽  
Yousuke MATSUKUMA ◽  
Yutaka ABE ◽  
Hiromichi ADACHI

2005 ◽  
Vol 17 (6) ◽  
pp. 068101 ◽  
Author(s):  
Tatiana G. Elizarova ◽  
Ivan A. Shirokov ◽  
Salvador Montero

2011 ◽  
Vol 26 ◽  
pp. 1322-1329 ◽  
Author(s):  
Zhang Licong ◽  
Zhang Yulong ◽  
Xu Jingde ◽  
Yang Gengyu ◽  
Hou Shiqiang ◽  
...  

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