The pressure and massflow ratio calculated by the 2D Navier-Stokes code were obtained exactly as in the experiment by increasing the inlet back-pressure until the internal shock system was expelled (inlet unstart). The results of theanbsp;...
|Title||:||Concepts avancés et les commandes des nouveaux moteurs d'avion|
|Author||:||North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium|