Browsing Aeronautical Research Council by Author "R. C. Hastings"

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The effect of a central jet on the base pressure of a cylindrical after-body in a supersonic stream

J. Reid; R. C. Hastings (1959)

This Report describes an experimental investigation of the factors affecting the base flow and jet structure behind a cylindrical after-body with a central nozzle. Seven interchangeable nozzles were tested. Six of these ...
Heat transfer in the vicinity of a 15 degrees compression corner at mach numbers from 2.5 to 4.4

R. C. Hastings; C. S. Brown; Susan Atkinson (1967)
A note on the interpretation of base pressure measurements in supersonic flows

R. C. Hastings (1958)
Turbulent boundary layers on a large flat plate at M = 4

R. C. Hastings; W. G. Sawyer (1970)

Transition positions, local skin-friction coefficients and boundary layer profiles measured in adiabatic flow on a flat plate are given. The data are for turbulent flow and cover a range of momentum-thickness Reynolds ...
Turbulent flow past two-dimensional bases in supersonic streams

R. C. Hastings (1963)

Experiments on the flow past two-dimensional, rearward-facing steps with turbulent approach boundary layers have been made at Mach numbers of 1.56, 2.41 and 3.10. Wide ranges of the ratio of boundary-layer thickness to ...

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