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Journal ArticleDOI

Investigation of supersonic nonisobaric jet structure

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This article is published in Tsagi Science Journal.The article was published on 2010-01-01. It has received 12 citations till now. The article focuses on the topics: Jet (fluid) & Supersonic speed.

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Citations
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Journal ArticleDOI

Shock-Wave Structure of Supersonic Jet Flows

TL;DR: In this paper, a brief overview of the studies of supersonic jet flows is given, with the aim of gaining experimental data on the formation of the shockwave structure and jet mixing layer in such flows.
Journal ArticleDOI

Gasdynamic structure of an axisymmetric supersonic underexpanded jet

TL;DR: The steady state structure of supersonic underexpanded jet flow at Ma = 1 is investigated in this article, where the measured total pressure distributions are presented in different cross sections and along the jet axis.
Journal ArticleDOI

Intensity fluctuations of a laser beam propagating through a supersonic flooded jet

TL;DR: In this article, the results of experimental researches of intensity fluctuations of a laser beam propagating through a supersonic flooded jet are presented and the inner scale of turbulence is estimated.
Proceedings ArticleDOI

Flow structure behind the Mach disk in supersonic non-isobaric jet

TL;DR: In this paper, the flow structure behind the Mach disk in the first cell of free supersonic underexpanded jets exhuasting from nozzles of different geometric Mach numbers at nozzle exit was examined.
Proceedings ArticleDOI

Determination of the gas-dynamic flow parameters by the PIV measurements

TL;DR: In this paper, a method of calculating the pressure from the velocity field measurement data by using the PIV contactless technique is considered, and the pressure distribution was calculated by using a pressure sensor.
References
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Journal ArticleDOI

Acoustics and Thrust of Quiet Separate-Flow High-Bypass-Ratio Nozzles

TL;DR: In this article, the authors demonstrate that modie cations of the core nozzle are generally more advantageous than of the fan nozzle, and demonstrate that the benefits of simultaneous modiecation of both nozzles are greater than those of chevrons.
Journal ArticleDOI

Structure of Supersonic Twin Jets

TL;DR: In this paper, the flow characteristics of coupled oscillatory motion of M j = 1.5 supersonic twin jets were described using the particle image velocimetry measurements, and a control technique using microjets placed at the nozzle exit was used to suppress the unsteady flow.