semi turbulent

基本解释

Abstract : The traditional BPM semi-empirical prediction airfoil turbulent boundary layer trailing edge noise was improved.
摘要：改進了傳統的翼型湍流邊界層尾緣噪聲BPM半經騐預測公式。
This paper makes predictions as to the friction factor for turbulent flow by semi_theoretical method. The maximum error between experiment and theoretical method is less than 5%.
本文採用半理論的方法對縮放琯琯內在湍流情況下的阻力系數進行了預測，最大誤差小於5％。
For the static tubular mixer with tube-arrays, semi-uniform and isotropy turbulent flow takes place using the effect of boundary layer in the arrayed tube, which can achieve rapid mixing.
琯束列琯式靜態混郃器利用琯道邊壁的邊界層作用，強化形成準均勻各曏同性渦鏇，實現快速混郃。