Browsing Aeronautical Research Council Reports & Memoranda by Author "F. Walkden"

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The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow

J. H. B. Smith; J. A. Beasley; Diana Short; F. Walkden (1965)

According to the linearized theory of supersonic flow, both the local slope of the mean surface of a wing producing a specified distribution of lift and the pressure on a wing due to a specified distribution of volume are ...
The equations of motion of a viscous compressible gas referred to an arbitrarily moving co-ordinate system

F. Walkden (1966)

Under review
A form of the supersonic flow equations for an ideal gas

F. Walkden (1972)

Non-linear partial differential equations that govern the steady supersonic three-dimensional flow of an inviscid ideal gas with constant specific heats in an arbitrary curvilinear co-ordinate space are derived. A special ...
A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow

R. H. Eldridge; F. Walkden (1966)

Summary. The equations of motion for supersonic flow over a symmetrical wing at zero incidence are linearised and the pressure coefficient at a point in the wing mean plane is expressed in terms of the finite part of a ...

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