Browsing Aeronautical Research Council (1945-1979) by Author "P. G. Pugh"

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Experimental verification of predicted static hole size effects on a model with large streamwise pressure gradients

P. G. Pugh; J. W. Peto; L. C. Ward (1971)
Measurements of pitching-moment derivatives for blunt-nosed aerofoils oscillating in two-dimensional supersonic flow

P. G. Pugh; L. Woodgate (1961)

Direct pitching-moment derivatives have been measured using the method of Scruton, Woodgate et al for two single-wedge blunt-nosed aerofoils. These measurements were made at Mach numbers of 1.75 and 2.47 and frequency ...
Notes on the automatic control of a blowdown wind tunnel

P. G. Pugh; L. C. Ward (1966)

This report briefly describes salient results obtained during commissioning Or the stagnation pressure control system of the N.P.L. 15 in x 10 in (38.1 cm x 25.4 cm) blowdown wind tunnel. The very different problems of low ...
A novel method for the estimation of the zero-lift forebody pressure drag of axisymmetric non-slender shapes at supersonic and hypersonic velocities

P. G. Pugh; L. C. Ward (1971)
A parametric study of the use of nose blunting to reduce the supersonic wave drag of forebodies

P. G. Pugh; L. C. Ward (1974)

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