![]() ![]() ![]() UNIT III NORMAL AND OBLIQUE SHOCKS 10 Governing equations – Variation of flow parameters across the normal and oblique shocks – Prandtl – Meyer relations – Use of table and charts – Applications. UNIT II FLOW THROUGH DUCTS 9 Flows through constant area ducts with heat transfer (Rayleigh flow) and Friction (Fanno flow) – variation of flow properties – Use of tables and charts – Generalised gas dynamics. ![]() UNIT I BASIC CONCEPTS AND ISENTROPIC FLOWS 6 Energy and momentum equations of compressible fluid flows – Stagnation states, Mach waves and Mach cone – Effect of Mach number on compressibility – Isentropic flow through variable ducts – Nozzle and Diffusers – Use of Gas tables. To gain some basic knowledge about jet propulsion and Rocket Propulsion. „h To understand the phenomenon of shock waves and its effect on flow. OBJECTIVE: „h To understand the basic difference between incompressible and compressible flow. ![]() ME2351 GAS DYNAMICS AND JET PROPULSION L T P C 3104 AIM: „h To impart knowledge to the students on compressible flow through ducts, jet propulsion and space propulsion. ![]()
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