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Normal Shock Inlet Oblique Shock Inlet All figures from Mattingly Elements of Gas Turbine Propulsion Seitzman Engine Inlets 1 AE4451 Propulsion Two dimensional mixed compression inlet Need fast reacting bypass doors Axisymmetric version central spike has weight advantage but 2 d simpler and gives more variation in air flow All figures from Mattingly Elements of Gas Turbine Propulsion Seitzman Engine Inlets 2 AE4451 Propulsion Po2 Poa Increasing Po loss from external oblique shocks Mach Number All figures from Mattingly Elements of Gas Turbine Propulsion Seitzman Engine Inlets 3 AE4451 Propulsion
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