Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels
Volf Ya. Borovoy,Vladimir Evguenyevich Mosharov,A. Noev,Vladimir Nikolaevich Radchenko +3 more
- Vol. 3, pp 15-24
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TLDR
In this paper, the application of temperature stenstive paint (TSP) technology for investigation of boundary layer transition in short-duration wind tunnels is presented. Investigations were made on sharp and blunted flat plates in UT-1 wind tunnel of TsAGI operated in Ludwieg scheme at Mach numbers 5, 6, and 8 (Reynolds numbers from 5.5 · 106 to 26 · 106 ).Abstract:
Application of Temperature Senstive Paint (TSP) technology for investigation of boundary layer transition in short-duration wind tunnels is presented. Investigations were made on sharp and blunted flat plates in UT-1 wind tunnel of TsAGI operated in Ludwieg scheme at Mach numbers 5, 6, and 8 (Reynolds numbers from 5.5 · 106 to 26 · 106 ). Both natural and induced boundary layer transitions were investigated.read more
Citations
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Experimental study of the laminar-turbulent transition on a blunt cone
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Two-Dimensional Shock-Wave/Boundary-Layer Interaction in the Presence of Entropy Layer
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Effect of Görtler-like vortices of various intensity on heat transfer in supersonic compression corner flows
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Three-dimensional shock-wave/boundary-layer interaction at the presence of entropy layer
Volf Ya. Borovoy,Ivan Vladimirovich Egorov,A. Maximenko,Vladimir Evguenyevich Mosharov,Vladimir Nikolaevich Radchenko,A. S. Skuratov,I. V. Struminskaya +6 more
TL;DR: In this paper, an experimental and numerical investigation of a gas flow on a flat plate near a single fin and a fin pair, generating crossings shocks, is performed, focused on the plate bluntness influence on the flow field and the heat transfer in the interaction region.
References
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Journal ArticleDOI
Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
TL;DR: In this paper, the authors reviewed the literature for transition on circular cones and scramjet forebodies from an experimental point of view, focusing on the effect of laminar-turbulent transition in hypersonic boundary layers.
Proceedings ArticleDOI
Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow
Journal ArticleDOI
Development of a high Reynolds number quiet tunnel for transition research
TL;DR: In this paper, the Taylor-Gortler vortices observed in a nozzle wall boundary layer were used to predict the limits of quiet performance for a proposed 20-in. quiet tunnel.
Journal ArticleDOI
Roughness Induced Transition Criteria for Space Shuttle-Type Vehicles
TL;DR: In this paper, the authors compared the impact of surface roughness on the performance of a delta wing shuttle orbiter with and without longitudinal pressure gradients on two-dimensional zero-pressure gradient flows and three-dimensional flows.
Proceedings ArticleDOI
Temperature sensitive paint (TSP) for heat transfer measurement in short duration wind tunnels
TL;DR: In this paper, temperature sensitive paint (TSP) technique was used to measure full-field surface heat transfer rates in short-duration wind tunnel and the results showed good repeatability but heat flux on the model nose was lower than CFD prediction and thermocouple measurement.