The performance of the turbojet engine is considerably affected by distorted
inlet flow.To the best of the authors' knowledge,there is no published
theoretical method for calculating the performance of an engine with distorted
inlet flow.Modifying the well-known“parallel compressor model”with a view
to making it applicable to the engine as a whole,the authors suggest a method
of calculation for predicting the engine operating point,as well as compressor
charac...
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