Browsing Aeronautical Research Council (1945-1979) by Author "I. M. Hall"

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An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream mach numbers between 0.8 and 1.41

E. W. E. Rogers; I. M. Hall; C. J. Berry (1960)

Summary. A study has been made of the flow development over the wing as the incidence and stream Mach number vary and this is illustrated by surface pressure distributions and oil-flow patterns. The growth and movement of ...
The operation of the N.P.L. 18 inches x 14 inches wind tunnel in the transonic speed range

I. M. Hall (1957)
Part I The Flow Pattern on a Tapered Sweptback Wing at Math Numbers between 0.6 and 1.6 Part II Experiments with a Tapered Sweptback Wing of Warren I 2 Planform at Mach Numbers between 0.6 and 1.6

I. M. Hall; E. W. E. Rogers (1960)

PART I. The development of the flow pattern on a swept wing with incidence and stream Mach number is described. The wing, of aspect ratio 2.828, taper ratio 0.333 and leading-edge sweep 53.5 deg, was tested at Mach numbers ...
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel

E. W. E. Rogers; I. M. Hall (1959)
Wall interference at transonic speeds on a hemisphere-cylinder model

E. W. E. Rogers; I. M. Hall (1960)

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