Quantitative density measurement of wake region behind reentry capsule (Improvements in accuracy of 3D reconstruction by evaluating the view-angle of measurement system)
IntroductionThe development of supersonic airplanes and rockets has been active all over the world. They are mainly designed and developed by using computational fluid dynamics (CFD). In order to assure the accuracy of CFD, experiments using supersonic wind tunnels, shock tubes, and ballistic ranges are being conducted, and quantitative density measurements
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