Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback

Table 1

Relevant design parameters of the compressor blade.

Number	1	2	3	4	5	6	7	8	9
Total pressure recovery coefficient ratio	1	0.994	0.985	0.977	0.971	0.965	0.961	0.944	0.903
Normal shock position	-0.15	-0.087	0.045	0.204	0.417	0.438	0.503	0.805	0.943