International Journal of Aerospace Engineering / 2017 / Article / Tab 7

Research Article

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

Table 7

Regression rate changes due to swirl flow.

Test #
(mm/s)

(mm/s)

(%)

1-S4A10.640.8533.00
2-S4A10.600.6713.56
3-S4A10.580.603.80
4-S4A10.610.7218.33

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