Heat removing under hypersonic conditions

被引：0
|
作者：
Semenov, Mikhail E. [1 ,2 ,3 ]
Nesterov, Victor A. [4 ]
Kuznetsov, Ilya E. [1 ]
Solovyov, Andrey M. [2 ]
Meleshenko, Peter A. [1 ,2 ]
机构：
[1] Zhukovsky Gagarin Air Force Acad, Starykh Bolshevikov St 54 A, Voronezh 394064, Russia
[2] Voronezh State Univ, Digital Technol Dept, Univ Skaya Sq 1, Voronezh 394006, Russia
[3] Voronezh State Univ Architecture & Civil Engn, 20 Letiya Oktyabrya St 84, Voronezh 394006, Russia
[4] Natl Res Univ, Moscow Aviat Inst, Volokolamskoe Shosse 4, Moscow 125993, Russia
来源：
CSNDD 2016 - INTERNATIONAL CONFERENCE ON STRUCTURAL NONLINEAR DYNAMICS AND DIAGNOSIS | 2016年 / 83卷
关键词：
THERMAL-STRESSES;
D O I：
10.1051/matecconf/20168307004
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
In this paper we consider the heat transfer properties of the axially symmetric body with parabolic shape at hypersonic speeds (with a Mach number M > 5). We use the numerical methods based on the implicit difference scheme (Fedorenko method) with direct method based on LU-decomposition and iterative method based on the Gauss-Seigel method. Our numerical results show that the heat removing process should be performed in accordance with the nonlinear law of heat distribution over the surface taking into account the hypersonic conditions of motion.
引用
收藏
页数：4
相关论文
共 50 条
  • [31] HEAT EXCHANGE MODELING ON THE AIRCRAFT SURFACE UNDER HYPERSONIC SPEED OF THE APPROACH FLOW
    Chernykh, A. A.
    Sharapov, A., I
    Peshkova, A., V
    Shatskikh, Y., V
    INTERNATIONAL TRANSACTION JOURNAL OF ENGINEERING MANAGEMENT & APPLIED SCIENCES & TECHNOLOGIES, 2019, 10 (05): : 689 - 694
  • [32] Mathematical modeling and simulation of porosity on thermomechanical properties of UHTCs under hypersonic conditions
    Zuccarini, Carmine
    Ramachandran, Karthikeyan
    Russo, Stefano
    Jayakody, Yasith C.
    Jayaseelan, Doni Daniel
    INTERNATIONAL JOURNAL OF CERAMIC ENGINEERING AND SCIENCE, 2023, 5 (01):
  • [33] Numerical simulation of transpiration cooling in porous nose cone under hypersonic conditions
    Pan, Mingjun
    Zhou, Qiang
    Huang, Zheqing
    Applied Thermal Engineering, 2024, 246
  • [34] An Evaluation Model of Star Sensor Observation Capability Under Hypersonic Aerothermal Conditions
    Chen, Bing
    Zheng, Yong
    Xu, Bin
    Li, Chonghui
    Ge, Fengna
    IEEE ACCESS, 2023, 11 : 646 - 654
  • [35] Numerical simulation of transpiration cooling in porous nose cone under hypersonic conditions
    Pan, Mingjun
    Zhou, Qiang
    Huang, Zheqing
    APPLIED THERMAL ENGINEERING, 2024, 246
  • [36] FIRST COLLISION CALCULATION OF CONE DRAG UNDER HYPERSONIC RAREFIED FLOW CONDITIONS
    LAURMANN, JA
    ASTRONAUTICA ACTA, 1967, 13 (04): : 401 - +
  • [37] Flow evolution of mixed layer on convex curvature wall under hypersonic conditions
    Zhang Zhen
    Yi Shi-He
    Liu Xiao-Lin
    Chen Shi-Kang
    Zhang Zhen
    ACTA PHYSICA SINICA, 2024, 73 (10)
  • [38] Numerical investigation on transpiration cooling with coolant phase change under hypersonic conditions
    Su, Hao
    Wang, Jianhua
    He, Fei
    Chen, Liang
    Ai, Bangcheng
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 129 : 480 - 490
  • [39] Unsteady simulation of hypersonic flow around a heat flux probe in ground testing conditions
    Bensassi, K.
    Lani, A.
    Rambaud, P.
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 113 : 889 - 897
  • [40] Removing dysfunctional mitochondria from axons independent of mitophagy under pathophysiological conditions
    Lin, Mei-Yao
    Cheng, Xiu-Tang
    Xie, Yuxiang
    Cai, Qian
    Sheng, Zu-Hang
    AUTOPHAGY, 2017, 13 (10) : 1792 - 1794
12345