Pressure Distribution Measurement around Hypersonic Delta-Winged Semicone : Measurement by Means of Magnetic Tape
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概要
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This paper describes measurements of pressure distribution around a semicone with a delta wing traveling at the hypersonic speed of Mach 10. The semiapex angles of the delta wing and semicone are 30 deg and 15 deg, respectively. The measurements are carried out under the conditions in which the angles of attack are 0 deg, 10 deg, and 20 deg. In this study, the pressure distribution measuring method using magnetic tape has been improved to be suitable for measuring pressure distribution around hyper-sonic vehicles. The pressure distributions are measured by utilizing the improved method.
- 一般社団法人日本機械学会の論文
- 1994-08-15
著者
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Nishio M
Department Of Mechanical Engineering Fukuyama University
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Nishio Masatomi
Department Of Mechanical Engineering Fukuyama University
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Kotake Mutsuo
Department of Aerospace Engineering, National Defense Academy
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Kotake Mutsuo
Department Of Aerospace Engineering National Defense Academy
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- The First Electric Discharge Method for Visualizing Three-Dimensional Shock Shapes Around Hypersonic Vehicles
- A Method for Measuring Fluid Pressure Using Magnetic Tape
- Second Electric Discharge Method for Visualizing Three-dimensional Shock Shapes around Hypersonic Vehicles
- Original Method for Visualizing Streamlines Around Hypersonic Vehicles