Results 61 to 70 of about 81,739 (264)
This paper reviews the state of phosphor thermometry, focusing on developments in the past 15 years. The fundamental principles and theory are presented, and the various spectral and temporal modes, including the lifetime decay, rise time and intensity ...
Konstantinos Kontis +1 more
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Assessment of Numerical Method by Experimental Data for Integrated Hypersonic Vehicles
This paper addresses the problem of rapid aerodynamic assessment and experimental verification of integrated hypersonic vehicles. Based on the adaptive Cartesian grid system, the aerodynamic performance of the air-breathing hypersonic vehicle is ...
X. Wen, J. Liu, Z. Liu, Z. Xia, L. Jin
doaj
An optical fiber balance for short-time wind tunnel force measurement of large-scale scramjet models
The scale of a scramjet has a profound impact on its combustion characteristics, and accurately replicating the integrated coupling dynamics between an aircraft and a scramjet in wind tunnel tests remains a significant challenge.
Bin Xu, Shien Yu, Jianzhong Zhang
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Effect of Wavy Wall on the Stability of Conical Hypersonic Boundary Layer at Small Angle of Attack
In order to obtain a high lift-drag ratio, hypersonic vehicles usually fly with a certain angle of attack. As a potential means to delay hypersonic boundary layer transition at 0° angle of attack, it is not clear how wavy wall affect the deve-lopment of ...
Chengjian ZHANG +4 more
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Application of Different PDF Models for Numerical Simulation of Scramjet
Since the turbulence-combustion interaction is of great influence on complex supersonic combustion field, the different distribution of probability density function(PDF) models is studied on the basis of assumed PDF models.
Ding Haixin, Zhong Chengwen
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The novel active flow control technology based on plasma synthetic jet (PSJ) has great application potential in the field of shock wave control due to its advantages such as no gas source, strong control ability, and wide excitation frequency band.
Wei XIE +5 more
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The problem of the delaying laminar to turbulent transition by the passive porous coating on the sharp cone at the angle of attack has been studied for the first time.
Morozov Sergey +2 more
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A Numerical Simulation of Hypersonic Wind Tunnel Flow.
In our country, some hypersonic wind tunnels for development of space planes and supersonic transports are now under construction and planned to construct. For designing these wind tunnels, it is indispensable to make use of CFD technology. This paper describes the results of a numerical simulation of the flow passage of a hypersonic wind tunnel.
Takashi Kawashima +3 more
openaire +2 more sources

