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|Document Type: ||Report|
|Title: ||The laminar boundary layer in slip flow|
|Authors: ||Nonweiler, T.|
|Issue Date: ||Nov-1952|
|Abstract: ||This report discusses the effects of the existence of a small, but finite, molecular mean-free-path on the steady air flow in the laminar boundary later. The boundary conditions at the exposed surface are modified by the existence of a slip velocity and temperature-jump between the air and the surface, and a theory of first-order approximation is developed to account for the consequent modification to the shear stress and heat flux to the surface. Continues…|
|Appears in Collections:||College of Aeronautics Reports|
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