Optimization of Temperature Sensitive Paint Formulation for Cryogenic Wind Tunnels

Journal of the Visualization Society of Japan ◽

10.3154/jvs.22.1supplement_321 ◽

2002 ◽

Vol 22 (1Supplement) ◽

pp. 321-324 ◽

Author(s):

Yoshimi IIJIMA ◽

Yasuhiro EGAMI ◽

Keisuke ASAI

Keyword(s):

Wind Tunnels ◽

Temperature Sensitive ◽

Paint Formulation ◽

Temperature Sensitive Paint

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Optimization of temperature-sensitive paint formulation for large-scale cryogenic wind tunnels

20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. ◽

10.1109/iciasf.2003.1274854 ◽

2004 ◽

Author(s):

Y. Iijima ◽

Y. Egami ◽

A. Nishizawa ◽

K. Asai ◽

U. Fey ◽

...

Keyword(s):

Large Scale ◽

Wind Tunnels ◽

Temperature Sensitive ◽

Paint Formulation ◽

Temperature Sensitive Paint

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Development of Temperature Sensitive Paint Formulation for Large Scale Cryogenic Wind Tunnels

Journal of the Visualization Society of Japan ◽

10.3154/jvs.24.supplement1_383 ◽

2004 ◽

Vol 24 (Supplement1) ◽

pp. 383-386 ◽

Author(s):

Yoshimi IIJIMA ◽

Hirotaka SAKAUE ◽

Yasuhiro EGAMI ◽

Akira NISHIZAWA ◽

Keisuke ASAI ◽

...

Keyword(s):

Large Scale ◽

Wind Tunnels ◽

Temperature Sensitive ◽

Paint Formulation ◽

Temperature Sensitive Paint

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Temperature sensitive paint (TSP) for heat transfer measurement in short duration wind tunnels

20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. ◽

10.1109/iciasf.2003.1274886 ◽

2004 ◽

Author(s):

V. Mosharov ◽

A. Orlov ◽

V. Radchenko

Keyword(s):

Heat Transfer ◽

Short Duration ◽

Wind Tunnels ◽

Temperature Sensitive ◽

Transfer Measurement ◽

Temperature Sensitive Paint ◽

Heat Transfer Measurement

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Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels

Progress in Flight Physics ◽

10.1051/eucass/201203015 ◽

2012 ◽

Author(s):

V. Borovoy ◽

V. Mosharov ◽

A. Noev ◽

V. Radchenko

Keyword(s):

Boundary Layer ◽

Short Duration ◽

Boundary Layer Transition ◽

Wind Tunnels ◽

Temperature Sensitive ◽

Layer Transition ◽

Temperature Sensitive Paint

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Temperature-Sensitive Paint Application in Cryogenic Wind Tunnels: Transition Detection at High Reynolds Numbers and Influence of the Technique on Measured Aerodynamic Coefficients

2007 22nd International Congress on Instrumentation in Aerospace Simulation Facilities ◽

10.1109/iciasf.2007.4380904 ◽

2007 ◽

Author(s):

U. Fey ◽

Y. Egami ◽

C. Klein

Keyword(s):

Reynolds Numbers ◽

Wind Tunnels ◽

Temperature Sensitive ◽

Aerodynamic Coefficients ◽

High Reynolds Numbers ◽

Temperature Sensitive Paint ◽

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Thermophysical Properties of Temperature Sensitive Paint

2018 Joint Thermophysics and Heat Transfer Conference ◽

10.2514/6.2018-3268 ◽

2018 ◽

Author(s):

Wit Stryczniewicz ◽

Andrzej J. Panas ◽

Robert Szczepaniak

Keyword(s):

Thermophysical Properties ◽

Temperature Sensitive ◽

Temperature Sensitive Paint

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Use of a Ring Wing Model to investigate Factors affecting Transition Measurement using Temperature Sensitive Paint and Hot Films in Transonic Flow

55th AIAA Aerospace Sciences Meeting ◽

10.2514/6.2017-1217 ◽

2017 ◽

Author(s):

Andrea Ciarella ◽

Simon Lawson

Keyword(s):

Transonic Flow ◽

Temperature Sensitive ◽

Factors Affecting ◽

Temperature Sensitive Paint

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Pressure sensitivity of a ruthenium complex based temperature-sensitive paint and its effect on heat flux determination in high-speed flows

Measurement Science and Technology ◽

10.1088/1361-6501/abff82 ◽

2021 ◽

Author(s):

Xu Liu ◽

Feng Gu ◽

Yingzheng Liu ◽

Di Peng

Keyword(s):

Heat Flux ◽

Ruthenium Complex ◽

Temperature Sensitive ◽

Pressure Sensitivity ◽

Temperature Sensitive Paint ◽

High Speed Flows ◽

Flux Determination

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Heat-Flux Measurements with Temperature-Sensitive Paint in a Mach-6 Quiet Tunnel

Journal of Spacecraft and Rockets ◽

10.2514/1.a32311 ◽

2013 ◽

Vol 50 (2) ◽

pp. 282-293 ◽

Author(s):

Tianshu Liu ◽

Christopher A. C. Ward ◽

Justin Rubal ◽

John P. Sullivan ◽

Steven P. Schneider

Keyword(s):

Heat Flux ◽

Temperature Sensitive ◽

Flux Measurements ◽

Temperature Sensitive Paint

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Visualization of Hypersonic Boundary Layer Transition on Elliptic Cone in High Enthalpy Shock Tunnel with Temperature-Sensitive Paint

54th AIAA Aerospace Sciences Meeting ◽

10.2514/6.2016-0358 ◽

2016 ◽

Author(s):

Takehiro Nagayama ◽

Hiroki Nagai ◽

Hideyuki Tanno ◽

Tomoyuki Komuro

Keyword(s):

Boundary Layer ◽

Shock Tunnel ◽

Boundary Layer Transition ◽

Temperature Sensitive ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

High Enthalpy ◽

Elliptic Cone ◽

Temperature Sensitive Paint ◽

High Enthalpy Shock Tunnel

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