2009 Fiscal Year Final Research Report
High-accuracy estimation of aerodynamic heating in high enthalpy flowusing Temperature-Sensitive Paint and Inverse method
Project/Area Number |
20760545
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Research Category |
Grant-in-Aid for Young Scientists (B)
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Allocation Type | Single-year Grants |
Research Field |
Aerospace engineering
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Research Institution | Tohoku University |
Principal Investigator |
NAGAI Hiroki Tohoku University, 大学院・工学研究科, 准教授 (70360724)
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Project Period (FY) |
2008 – 2009
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Keywords | 感温塗料 / 空力加熱率 / 高エンタルピ流 |
Research Abstract |
The objective of this study is the establishment of aerodynamic heating measurement technique using Temperature-Sensitive Paint (TSP) in high enthalpy flow with self-luminescence such as an atmospheric re-entry vehicle. First of all, the effect of model material, thickness and the limitation of spatial resolution for the heat flux distribution estimation were evaluated by laser heating test. In addition, TSP characteristics were investigated for the sensitivity with the different thickness and material, the response, the degradation. Then, this technique was applied to hypersonic wind tunnel test and the accuracy was evaluated. The results demonstrated the validity of TSP technique for aerodynamic heating measurement.
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Research Products
(16 results)
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[Presentation] Application of Temperature-Sensitive Paint to Heat Flux Measurement in High Temperature Gas Flow, 2-52009
Author(s)
Ha S., Sawamura, R., Sakamoto, H., Nagai, H., Numata, D., Asai, K.
Organizer
6h International Conference on Flow Dynamics
Place of Presentation
Sendai, Japan.
Year and Date
2009-11-04
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[Presentation] Surface heat flux visualization on a blunt-nosed body with an aerospike in hypersonic flow using Temperature-Sensitive Paint2009
Author(s)
Nagai, H., Ha, S., Asai, K., Tsuboi, N., Nakakita, K.
Organizer
27th International Symposium on Space Technology and Science, 2009-e-27
Place of Presentation
Tsukuba, Japan
Year and Date
2009-07-10
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