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With the invention of the aircraft, it has become much faster and larger than the original Wright Brothers aircraft. When the speed is high enough to cross the speed of sound, air conditions will be different than that in low speed due to the existence of shock wave. In this work, we introduce several numerical ways to analyze the performance of the airfoil when the speed is higher than the speed of sound. With these numerical methods, we analyzed the performance of diamond-shaped airfoil under different angles of attack and speed. With this data, engineers can choose a better airfoil to attain a lower drag coefficient as well as lift coefficient when designing a high-speed aircraft.
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篇名 Study on Aerodynamic Characteristics of Supersonic Airfoil
来源期刊 现代机械工程(英文) 学科 物理学
关键词 Aerodynamic SUPERSONIC SPEED Diamond-Shape AIRFOIL Drag COEFFICIENT LIFT COEFFICIENT
年,卷(期) 2019,(1) 所属期刊栏目
研究方向 页码范围 13-19
页数 7页 分类号 O35
字数 语种
DOI
五维指标
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研究主题发展历程
节点文献
Aerodynamic
SUPERSONIC
SPEED
Diamond-Shape
AIRFOIL
Drag
COEFFICIENT
LIFT
COEFFICIENT
研究起点
研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
现代机械工程(英文)
季刊
2164-0165
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
141
总下载数(次)
0
总被引数(次)
0
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