Titlebook: Numerical and Physical Aspects of Aerodynamic Flows; Tuncer Cebeci Conference proceedings 1982 Springer Science+Business Media New York 19

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泰然自若

Experiments on Initial and Boundary Conditionsntal interferences. Data obtained by the Wright brothers in their historic wind tunnel enabled them to evaluate the possibility of flying; by current standards they would probably not even fit in what engineers call the “ballpark” range. The designer’s problem is efficiency; errors larger than 1% in

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Popcorn

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Some Observations on Numerical Solutions of the Three-Dimensional Navier-Stokes Equationsions. These flows may be either laminar or turbulent or both, and for laminar flow the use of the three-dimensional Navier-Stokes equations is required to adequately represent the motion. For turbulent flows, these same equations are usually ensemble-averaged, and with the introduction of current-ge

無節(jié)奏

Some Recent Studies in Triple-Deck Theorya continual challenge to theoreticians for many years. The usual approach, and one which I favor, is to regard it as controlled by an interaction between an external inviscid and a viscous boundary layer. For some time the discovery [2.8] that a laminar boundary layer invariably appears to become si

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gerrymander

Nonasymptotic Theory of Unseparated Turbulent-Boundary-Layer — Shock-Wave Interactions with Applicat turbomachinery and air-breathing-engine inlets and diffusors. Of particular importance are the features of upstream influence, boundary-layer displacement, skin friction, and incipient separation dominated by the thin interactive shear-stress disturbance layer very close to the surface. Lighthill’s

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