Browsing Aeronautical Research Council (1945-1979) by Author "B. M. Davis"

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The change of pitot pressure across oblique shock waves in a perfect gas

W. J. Graham; B. M. Davis (1965)
An experimental investigation of the interaction between a forward-facing step and a laminar boundary layer in supersonic, low-density flow

E. W. E. Rogers; C. J. Berry; B. M. Davis (1965)

The present research programme of the National Physical Laboratory is concerned with the influence exerted on model forces and surface pressures by the thick, laminar boundary layers characteristic of rarefied, near-continuum ...
Experiments with cones in low-density flows at mach numbers near 2

E. W. E. Rogers; C. J. Berry; B. M. Davis (1964)

Summary. Tests have been made on the N.P.L. low-density tunnel on two pressure-plotting cones of 15 deg and 30 deg semi-vertex angle placed at zero incidence to the flow. The stream static pressure was varied between 20 ...
An investigation of the flow about circular cylinders placed normal to a low-density, supersonic stream

S. C. Metcalf; C. J. Berry; B. M. Davis (1964)

The pressure distribution around circular cylinders has been measured near M∞ = 2, for Reynolds numbers between 5 and 135. The induced pressure due to viscous effects has been estimated using a 'tangent-cylinder' method ...
A note on turbulent boundary-layer allowances in supersonic nozzle design

E. W. E. Rogers; B. M. Davis (1957)

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