International Journal of Aerospace Engineering / 2018 / Article / Tab 4

Research Article

Propulsive Efficiency of Ridge/Inlet Configuration

Table 4

Shape factor and flow separation coordinate.

for inlet for ridge/inlet for inlet for ridge/inlet

0.33.5012.3410.156
0.53.0682.4810.177
0.83.8042.6630.2030.139

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