Войти
  • 2842Просмотров
  • 8 месяцев назадОпубликованоEvan K

Gas Turbine Engine Axial Compressor Velocity Triangles

Clearing up a topic after a professor presented it in a difficult way. This is how to determine if a compressor "stage" (a rotor and stator pair) is viable or not, depending on the angle of the blades in each and the direction of the rotors rotation velocity. This may be imperfect, but it's better than what we were given in class.