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- W2084875522 abstract "5for three different jet momentum coefficients: C� � 0:02, 0.04, and 0.16. Some numerical computations are used to assesstheextenttowhichtheyareadequateforengineeringanalysisanddesignofthecoflow-jetmethod.Theresults clearly demonstrate the lift augmentation capability, particularly at high incidence angles. The increase in lift and stall margin depends on the momentum coefficient, and for the range tested, the increase in the integral of the airfoil static pressure distribution varies from 40 to 100%. The results suggest that the coflow-jet airfoil is more effective whenbothinjectionandsuctionareusedsimultaneously,comparedwiththecaseinwhichtheyareindividuallyused. A first-order analysis of the combined merits of injection and suction indicate that these processes are not strongly coupled to each other and thus may possibly be analyzed separately." @default.
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- W2084875522 date "2009-01-01" @default.
- W2084875522 modified "2023-10-01" @default.
- W2084875522 title "Flow Control of an Airfoil via Injection and Suction" @default.
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- W2084875522 doi "https://doi.org/10.2514/1.38394" @default.
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