M E 381P.2
Compressible Flow and Turbomachinery
Two-dimensional flow at subsonic and supersonic Mach numbers, method of characteristics, shock tubes, oblique shocks, wave interactions.
Prerequisites & course information
Two-dimensional flow at subsonic and supersonic Mach numbers, method of characteristics, shock tubes, oblique shocks, wave interactions.
Sources
- Course catalogue ↗2026-2027