Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations
Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations
Details
- OL Work ID
- OL11302230W
Subjects
Viscous flowData processingRamjet enginesMathematical modelsMathematicl modelsAirplanesNavier-Stokes equations