...
机译:射流到靶板的距离和孔间距的变化对冲击阵列传热的横流影响
Parks College of Engineering, Aviation, and Technology, Saint Louis University, 3450 Lindell Boulevard, St. Louis, MO 63103, USA;
Parks College of Engineering, Aviation, and Technology, Saint Louis University, 3450 Lindell Boulevard, St. Louis, MO 63103, USA;
Oliver L. Parks Endowed Chair, Parks College of Engineering, Aviation, and Technology, Saint Louis University, 3450 Lindell Boulevard, St. Louis, MO 63103, USA;
Department of Mechanical and Automotive Engineering, High Safety Vehicle Core Technology Research Center, Inje University, 197 Inje-ro, Gimhae, Gyeongnam 621-749, Republic of Korea;
Aero/Thermal & Heat Transfer, Solar Turbines, Inc. 2200 Pacific Highway, P.O. Box 85376, Mail Zone C-9, San Diego, CA 92186-5376, USA;
Aero/Thermal & Heat Transfer, Solar Turbines, Inc. 2200 Pacific Highway, P.O. Box 85376, Mail Zone C-9, San Diego, CA 92186-5376, USA;
Impinging jet; Impingement jet array cooling; Jet-to-target plate distance; Jet hole spacing; Nusselt number;
机译:射流阵列撞击冷却局部螺母数变化:射孔阵列间距,射流至靶板间距和雷诺数的影响
机译:射流至靶板的距离和雷诺数对射流阵列撞击传热的影响
机译:射流与靶板间距低时,废空气去除方案对撞击-排放系统中的内部传热的影响
机译:射流阵列撞击冷却产生的横流:射孔阵列间距,射流到靶板距离和雷诺数的影响
机译:射流阵列冲击传热:马赫数,雷诺数,温度比和孔间距的单独影响。
机译:TiO2纳米溶液浓度对加热铝板双撞击射流传热增强的影响
机译:横流射流冲击冷却加热障碍物在线阵列传热与压降的数值研究
机译:射流阵列冲击流动分布和传热特性。初始横流和非均匀阵列几何的影响。