Browsing by Author "C. R. Taylor"

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Measurements, at mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings

C. R. Taylor (1961)

Measurements have been made of the longitudinal characteristics of one plane and three cambered slender ogee wings at two subsonic and eight supersonic Mach numbers up to 2.8. The tests also included measurements of the ...
A subsonic lifting-surface theory for low-aspect-ratio wings

C. R. Taylor (1956)

A method is developed for determining the loading on low-aspect-ratio wings. By allowing for down stream effects on the flow at a station on the wing and for the trailing-edge condition, the method improves on R. T. Jones's ...
Super VC 10 cruise drag - a wind tunnel investigation part 1 experimental techniques

C. R. Taylor; J. R. Hall; R. W. Hayward (1970)
Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7

C. R. Taylor; T. A. Cook (1965)
Wind-tunnel tests on a 30 per cent. suction wing

E. J. Richards; W. S. Walker; C. R. Taylor (1945)

Tests carried out on a 16 per cent. suction wing have shown that it is impossible to maintain laminar flow aft of the suction slot at high Reynolds numbers, because of the dynamic instability of the laminar layer over the ...

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