次世代スペースシャトルの試験機X-33周りの流れの放電発光法による可視化 [in Japanese] Visualization of Flowfield around X-33 Test Vehicle Utilizing Electric Discharge Method [in Japanese]
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Visualizations of flowfield around the X-33 test vehicle have been performed utilizing the electric discharge method. The electric discharge method has been invented and developed by the authors and others for visualizing three dimensional hypersonic flowfield phenomena. In this experiment the objectives of visualization are three dimensional shock shapes, temperature distributions, and flow patterns near the model surface. It is considered that these visualized results are useful for verifying the theoretical and numerical results of the flowfield around the model. These visualizations are carried out using the hypersonic gun tunnel whose main characteristics are that the Mach number is 10 and the duration is 10ms.
- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 47(544), 210-216, 1999-05
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES