|
This article is cited in 2 scientific papers (total in 2 papers)
Investigation of supersonic underexpanded jets exhausting into a slotted submerged space
S. P. Kiselev, V. P. Kiselev, V. N. Zaikovskii Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
Abstract:
Results of experimental and numerical modeling of supersonic under expanded jets exhausting into a slotted submerged space formed by two parallel disks are presented. It is demonstrated that the structure of the exhausting off-design jet depends on the distance between the disks. The friction force acting from the disks on the gas is responsible for significant changes in the supersonic jet structure. At a certain distance between the disks, there arises a curvilinear shock wave, followed by a subsonic flow region. In this case, the jet boundary acquires a fan-shaped structure rather than a typical barrel-shaped structure.
Keywords:
slotted space, plane channel, supersonic jet, shock wave, numerical simulation, difference scheme, experiment.
Received: 30.09.2019 Revised: 30.09.2019 Accepted: 30.09.2019
Citation:
S. P. Kiselev, V. P. Kiselev, V. N. Zaikovskii, “Investigation of supersonic underexpanded jets exhausting into a slotted submerged space”, Prikl. Mekh. Tekh. Fiz., 61:2 (2020), 81–91; J. Appl. Mech. Tech. Phys., 61:2 (2020), 225–234
Linking options:
https://www.mathnet.ru/eng/pmtf341 https://www.mathnet.ru/eng/pmtf/v61/i2/p81
|
Statistics & downloads: |
Abstract page: | 32 | Full-text PDF : | 3 | First page: | 1 |
|