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Advances in Aerodynamics

Table 1 Specifications of NASA Rotor 37

From: Static aeroelasticity analysis of a rotor blade using a Gauss-Seidel fluid-structure interaction method

Parameter

Value

Blade count

36

Design rotational speed (r/min)

17188.7

Design mass flow (kg/s)

20.19

Design pressure ratio

2.106

Design polytropic efficiency (%)

88.9

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