![]() It is a give and take situation, an aircraft engine, is a "comprimise" of circumstances as Roscoe says in the construction of an aircraft. This situation can occur and allow the engine to run optimally, (normally).Ĭlassic case, F-16, if you notice the upper lip of the inlet, the shock wave will form around that lip and keep the shock wave from entering the inlet, first stage and subsequent stages of the compressor. Obi - It is not always necessary to have a variable inlet geometry type situation so long as the shock wave does not enter the inlet, however, it is possible to have compressible flow enter and go through a process called diffusion, where the pressure increases, temperature decreases, and velocity decreases.
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