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Browsing by Author "Craven, A. H."

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A potential flow model for the flow about a nacelle with jet

Craven, A. H. (College of Aeronautics, Cranfield., )
An investigation of vortex breakdown at Mach 2

Craven, A. H.; Alexander, A. J. (College of Aeronautics, )

Wind tunnel tests have been made at M = 2 on a 75° swept delta wing in order to study the progressive breakdown of the leading edge vortices, which occurs at high incidence. The incidence at which vortex breakdown occurred ...
Base pressure at subsonic speeds in the presence of a supersonic jet

Craven, A. H.
Base pressure at supersonic speeds in the presence of a supersonic jet

Craven, A. H.; Chester, D. H.; Graham, B. H. (College of Aeronautics, )
Boundary layers with suction and injection a review of published work on skin friction

Craven, A. H. (College of Aeronautics, )
On the application of boundary layer control to a slender wing supersonic airliner cruising at M = 2.2

Craven, A. H.; Hopkins, H. L. (College of Aeronautics, )
The aerodynamic derivatives of an aerofoil oscillating in an infinite staggered cascade

Craven, A. H. (College of Aeronautics, )
The compressible laminar boundary layer with foreign gas injection

Craven, A. H. (College of Aeronautics, )
The effect of density on jet flow at subsonic speeds

Craven, A. H. (College of Aeronautics, )
The effect of jet deflection on the interference of a rearward facing jet

Craven, A. H. (College of Aeronautics, )
The flexure-torsion flutter of cambered aerofoils in cascade

Craven, A. H. (College of Aeronautics, Cranfield., )
The free streamline method applied to the flow at the rear of a duct

Craven, A. H. (College of Aeronautics, Cranfield, )
The interference of a rearward facing jet on the flow over three representative afterbody shapes in a uniform subsonic flow

Craven, A. H. (College of Aeronautics, )

Browsing by Author "Craven, A. H."

Browsing by Author "Craven, A. H."

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