International Journal of Aerospace Engineering / 2018 / Article / Tab 3

Research Article

Propulsive Efficiency of Ridge/Inlet Configuration

Table 3

Duct flow parameters.

inlet for inlet/ridge for ridge/inlet for inlet without ridge (%)

0.30.9910.9910.0340.351~0.0
0.50.9810.9850.0400.2395.1
0.80.9790.9890.1100.26212.7

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