Research Article
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 |
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