Quantitative Measurement of Supersonic Flow Field around an Asymmetric Cone Model with CGBOS Method and 3D-CT Reconstruction
スポンサーリンク
概要
- 論文の詳細を見る
- 2011-08-31
著者
-
Ota Masanori
Graduate School Of Engineering Chiba University
-
Maeno Kazuo
Graduate School And Faculty Of Engineering Chiba University
-
KATO Hiroko
Graduate School of Engineering, Chiba University
-
HAMADA Kenta
Graduate School of Engineering, Chiba University
-
NODA Ryusuke
Graduate School of Engineering, Chiba University
-
Noda Ryusuke
Graduate School Of Engineering Chiba University
-
Hamada Kenta
Graduate School Of Engineering Chiba University
-
Maeno Kazuo
Graduate School & Faculty Of Engineering Chiba University
-
Kato Hiroko
Graduate School Of Engineering Chiba University
-
Ota Masanori
Graduate School And Faculty Of Engineering Chiba University
-
Ota Masanori
Graduate School & Faculty Of Engineering Chiba University
関連論文
- High-Speed Visualization of Total Radiation and CARS Measurement of Vibrational/Rotational Temperatures behind Hypervelocity Shock Waves of 5km/s
- The LIF Measurement of Interaction of Gas Jet Flow with Plane Wall under Low Pressure Conditions
- Quantitative Measurement of Supersonic Flow Field around an Asymmetric Cone Model with CGBOS Method and 3D-CT Reconstruction
- Quantitative Measurement of Heat Flow in Natural Heat Convection Using Color-Stripe Background Oriented Schlieren (CSBOS) Method
- Small Model Experiment on the Pressure Wave Formation by Entering the Tunnel of Conventional Limited Express with Diaphragmless Driver Acceleration Apparatus
- Hybrid algebraic reconstruction technique for tomographic reconstruction of the wave interaction around a rectangular rod
- Quantitative Measurement of Natural Convection from Multiple Heat Sources using Color-Stripe Background Oriented Schlieren (CSBOS) CT Method
- The Spatial Distribution of Ro/Vibrational Temperatures for Nitrogen Molecules behind Hypervelocity Shock Waves by CARS Measurement
- Interferometric Computed Tomography Measurement and Novel Expression Method of Discharged Flow Field with Unsteady Shock Waves