Comments on Milgram: “Calculation of Attached or Partially Separated Flow Around Airfoil Sections”
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A Priori
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The title paper presents a relatively unified potential flow theory for attached and partially separated (trailing-edge separation) two-dimensional, incompressible airfoil sections. The partially separated flows are characterized by nonreattaching flow separation from a point on the suction side of the airfoil downstream from the leading edge; it is required that the location of this separation point and the corresponding separation pressure be specified a priori. Figures 5 and 6 of the subject paper present the test data and the theoretical results for the NACA 63–018 airfoil at 15- and 18-deg angle of attack, respectively, as the only experimental verification for partially separated flows.
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1999 ◽
Vol 103
(1023)
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pp. 237-244
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1967 ◽
Vol 27
(1)
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pp. 97-109
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1997 ◽
Vol 333
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pp. 403-413
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