2021
DOI: 10.1016/j.ijft.2021.100096
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Derivation of Navier–Stokes equation in rotational frame for engineering flow analysis

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Cited by 7 publications
(4 citation statements)
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“…Table 2 illustrates the investigation of the three moments in the CFD simulation cases, leading to the situations described in the aforesaid definitions. The mathematical expression of the idle and thrust moments with aspect to ω and U 1 is derived from the steady state and incompressible flow modified Navier-Stokes equations in the MRF form, containing the additional centrifugal force terms in the momentum conservation shown as Equation ( 12) [34]. The source term of the relative coordinate system is used to derive the expression of idle moment M Idle on the rotor plate through integration as Equation (13).…”
Section: Moment Analysis Methodsmentioning
confidence: 99%
“…Table 2 illustrates the investigation of the three moments in the CFD simulation cases, leading to the situations described in the aforesaid definitions. The mathematical expression of the idle and thrust moments with aspect to ω and U 1 is derived from the steady state and incompressible flow modified Navier-Stokes equations in the MRF form, containing the additional centrifugal force terms in the momentum conservation shown as Equation ( 12) [34]. The source term of the relative coordinate system is used to derive the expression of idle moment M Idle on the rotor plate through integration as Equation (13).…”
Section: Moment Analysis Methodsmentioning
confidence: 99%
“…The RANS mean mass and momentum transport equations in the moving rotational frame (MRF) system were written as Equations ( 13) and ( 14) in integral form. The steadystate and incompressible flow during the idle moment is governed by the modified Navier-Stokes equations in the MRF [38]. These equations include additional centrifugal force terms in the momentum conservation, resulting in the derivation of Equation ( 14) as Equation (15).…”
Section: Thrust and Idle Moment Equationmentioning
confidence: 99%
“…The two varying independent variables i.e., 𝑈 1 and 𝜔 comprise a dynamic Tip Speed Ratio (TSR) matrix using Eq. (10), shown for both turbines as Table 2a,b. The turbine's optimal TSR can be obtained by the Cp -TSR curve.…”
Section: Moment Analysismentioning
confidence: 99%