International Journal of Aerospace Engineering / 2017 / Article / Tab 1

Research Article

Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor

Table 1

Relative errors of test variables.

VariableRelative error

0.004
0.0001
0.0107
0.0004
0.002
0.01
0.0071
0.0001
0.0034
0.0208
0.0203
0.0209

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