Titlebook: Numerical and Phyical Aspects of Aerodynamic Flow III; Tuncer Cebeci Conference proceedings 1986 Springer-Verlag New York Inc. 1986 develo

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Laminar Separation Studied as an Airfoil Problemrfoils operating in the Reynolds-number (Re) range well below one million. This paper presents an aerodynamic theory of the laminar separation to further our understanding of the aerodynamic-flow behavior at Re = 10.–10., that is, at the lower end of this flight regime.

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A Comparison of Interactive Boundary-Layer and Thin-Layer Navier—Stokes Procedures generally be solved for flows where small-scale fluctuations are unimportant, emphasis has been placed on particular reduced forms such as those appropriate to regions of inviscid flow and boundary layers. In recent years, and with the application of numerical solution procedures in mind, attention

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Development of a Navier—Stokes Analysis to Investigate the Mechanism of Shock-Wave—Boundary-Layer Inbe completely analyzed. Since the interaction causes an abrupt pressure rise and boundary-layer thickening and may be accompanied by regions of local separation, the interaction flow can be a major contributor to the overall body drag and can cause substantial changes in the pressure distribution fr

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Unsteady Airfoil Boundary Layers—Experiment and Computationtrol surfaces. Several aspects of a representative unsteady flow about a fixed airfoil have been studied at M.I.T. The work has concentrated on obtaining experimental measurements of boundary layer and wake velocities in attached flow and surface pressure distributions in both attached and separated