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CFD evaluation of thermal convection inside the DACON convection sensor in actual space flight

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Figure

Figure 2. gx and gy and Tx and Ty from Previously Reported Results [3].
Figure 3. Meshed Cylindrical Air Filled Volume with Sensor Point Surfaces.
Figure 7. (a) Isotherms at the Sensor Plane [(0.0225 m, 0, 0.012 m), (0, 0.0225, 0.012), (0, 0.0225, 0.012)] at 390 s; (b) Velocity Contours at Sensor Plane[(0.0225 m, 0,0.012 m), (0, 0.0225, 0.012), (0, –0.0225, 0.012)] at 390 s; (c) Velocity Contours at
Figure 10. FFT of CFD Simulated Temperature Difference between Two Y Directional Sensor junctions in Astronaut Swung Experiment
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