1.

What is the static thrust for an engine as derived from the integral momentum equation?

A. T = \(\dot {m}\)ue + Ae(pe – p0)
B. T = \(\dot {m}\)Ae(pe – p0)
C. T = Ae(pe – p0)
D. T = \(\dot {m}\)Ae
Answer» B. T = \(\dot {m}\)Ae(pe – p0)


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