Receptivity Study of Hypersonic Boundary Layer under Freestream Finite Amplitude Continuous Entropy Disturbance with Single Frequency
Xiao-jun TANG1Hai-xia LI2Cai-yan TANG3Guo-bao DAI1
1. Beijing Spacecrafts,China Academy of Space Technology2. School of Mechanical and Electrical Engineering,North China Institute of Aerospace Engineering3. Nanjing global village Chancheng development co.LTD
摘要：The DNS method is used to calculate the unsteady flowfield around blunt cone under the action of a single frequency finite amplitude continuous entropy wave.The hypersonic flowfield response to single frequency finite amplitude entropy wave is investigated,and the hypersonic boundary layer receptivity features under single frequency finite amplitude disturbance are explored.The results find that the strong disturbance wave is produced by the interaction of freestream wave with shock wave and boundary layer,and there are regular high-entropy and low-entropy regions in the downstream evolution process.The frequency characteristics of boundary layer disturbance wave are directly related to freestream disturbance wave,and the frequency characteristics become weaker as the disturbance wave evolves downstream.During the development of disturbance downstream,the second,third and fourth（f2-f4） order modes in the boundary layer increase relatively.The central disturbance modes of the nose region are the fundamental mode in the boundary layer,and the main disturbance modes in the boundary layer of the downstream region of the flowfield are composed of the fundamental mode（f1） and the second,third and fourth（f2-f4） order modes.
会议名称：
2019 4th International Conference on Automation,Mechanical and Electrical Engineering（AMEE 2019）
会议时间：
2019-10-27
会议地点：
中国福建厦门
- 专辑：
基础科学; 工程科技Ⅱ辑
- 专题：
力学; 航空航天科学与工程; 航空航天科学与工程
- DOI：
10.26914/c.cnkihy.2019.055644
- 分类号：
V211;V411
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