6. Physics of a Fluid, Neutral and Ionized Gases

AN EXPERIMENTAL AND CFD INVESTIGATION OF A SUPERSONIC NONISOBARIC JET EXHAUSTING FROM A BEVELED NOZZLE

Valeriy I. Zapryagaev
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
zapr@itam.nsc.ru
Ivan N. Kavun
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
i_k@list.ru
Sergey G. Kundasev
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
kundasev.sergey@gmail.com
The material was received by the Editorial Board: 06.03.2014
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.

Keywords:
shock-wave structure, supersonic jet, beveled nozzle, experiment, CFD results, verification
УДК 533.6.011.5

AN EXPERIMENTAL AND CFD INVESTIGATION OF A SUPERSONIC NONISOBARIC JET EXHAUSTING FROM A BEVELED NOZZLE 
References: Zapryagaev V. I., Kavun I. N., Kundasev S. G. AN EXPERIMENTAL AND CFD INVESTIGATION OF A SUPERSONIC NONISOBARIC JET EXHAUSTING FROM A BEVELED NOZZLE . Vestnik NSU. Series: Physics. 2014, vol. 9, no. 2. P. 75–83 (in Russ.). DOI: 10.54362/1818-7919-2014-9-2-75-83