Supersonic Wind Tunnel - EPFL Rocket Team

Explores the performance advantages of convergent-divergent nozzles in supersonic applications.

Explores shock and expansion waves through animations, demonstrating their effects on air density and refractive index.

Explores straight shocks in fluid dynamics, discussing entropy, ideal gases, and the Rankine-Hugoniot relation.

Covers isentropic flows, Mach waves, and their interaction in supersonic flows.

Covers the Rocket Problem, exploring momentum diagrams, mass relations, rocket thrust, and providing a solution for no external forces.