The drag of an infinite swept wing is found in terms of the drag of a related unswept wing having the same relative position of transition. Results in incompressible flow are expressed in terms of a 'sweep factor'. Detailed ...
An attempt is made to estimate pressure distribution, tyre deflection and lift on a fully aquaplaning smooth tyre assuming an idealised non-viscous flow in front of the tyre followed by Stokes flow under the tyre. The ...
The boundary layer flow over a cone inclined at a small angle to a supersonic stream, and over a type of caret (Maikapar, Nonweiler) surface, as generalised by Townend, is calculated by an implicit finite difference method. ...