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Browsing Aeronautical Research Council (1945-1979) by Author "M. D. Dobson"

Now showing items 1-8 of 8

The external drag of fuselage side intakes rectangular intakes with compression surfaces vertical

M. D. Dobson (1974)
An investigation of the pressure distributions on a 45 degree swept half wing including the effects of upper surface spoilers

M. D. Dobson (1971)
Notes on the internal drag, lift and pitching moment of a ducted body

J. W. Britton; M. D. Dobson (1972)
Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing

M. D. Dobson (1970)
Wind tunnel tests at M = 2.0 on interference effects between intake flows in a four-engine nacelle

M. D. Dobson (1964)
Wind tunnel tests at supersonic speeds on a model of the fairey delta 2

M. D. Dobson (1964)
Wind tunnel tests between M = 0.4 and 2.0 on a cambered wing of slender ogee planform

M. D. Dobson; R. King-Underwood (1965)
Wind tunnel tests on a rectangular, twin duct, variable geometry air intake at supersonic speeds

M. D. Dobson (1967)

Now showing items 1-8 of 8

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