NACA 0012 // 0.8 Mach - Transonic Flight Shock waves. ergun umut kılınc 0:07 2 years ago 117 Скачать Далее
Shock wave due to supersonic flow over an airfoil. agermannamedhans 0:22 9 years ago 88 238 Скачать Далее
NACA 0012 Airfoil With 0.8 Mach and 5 Degree of Angle of Attack selin ş 1:41 2 years ago 30 Скачать Далее
Transonic Aerofoil CFD - NACA0012 Deceleration with OpenFOAM Sebastiano Stipa 0:11 3 years ago 1 010 Скачать Далее
Mach contours of transonic flow past NACA 0012 airfoil Sreejith N A 0:59 12 years ago 5 613 Скачать Далее
oscillation starts - shock buffeting on an airfoil rosa mojdehi 0:21 11 years ago 2 166 Скачать Далее
Mesh adaptation for NACA 0012 airfoil in supersonic flow UltraProQQQ 0:17 11 years ago 3 718 Скачать Далее
High Speed Flight : Part 2 - Transonic Flight National Aerospace Library 19:05 3 years ago 10 351 Скачать Далее
Transonic flow over NACA0012_AOA range 0 to 10_ANSYS CFX khider jabur 2:41 9 years ago 245 Скачать Далее
Drag-based adaptation for NACA 0012, 1.25 degrees angle of attack, Mach=0.8, Re=1e5, RANS-SA David Darmofal 0:08 4 years ago 512 Скачать Далее
2D URANS simulation of transonic flutter. ns mach m0 875fi1 930 Kartik Venkatraman 0:24 2 years ago 95 Скачать Далее
Angle of Attach Effect towards Flow Separation over NACA0012 Airfoil | Schlieren Visualization Luftvis Science 0:47 1 year ago 119 Скачать Далее