International Journal of Aerospace Engineering / 2018 / Article / Tab 1

Research Article

Propulsive Efficiency of Ridge/Inlet Configuration

Table 1

Example of acceptable residual accuracy for ridge/inlet configuration.

Number of iterationsContinuity velocity velocity velocityEnergy

20,0008.251 × 10−43.384 × 10−61.079 × 10−53.917 × 10−44.112 × 10−52.328 × 10−44.062 × 10−5

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