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Showing 10 out of a total of 10 results for collection: CoA. Reports. (0.009 seconds)

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Boundary layers with suction and injection a review of published work on skin friction

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

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

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

Craven, A. H. (College of Aeronautics, Cranfield, )
A potential flow model for the flow about a nacelle with jet

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

Craven, A. H. (College of Aeronautics, )
Base pressure at subsonic speeds in the presence of a supersonic jet

Craven, A. H.
The aerodynamic derivatives of an aerofoil oscillating in an infinite staggered cascade

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

Craven, A. H.; Chester, D. H.; Graham, B. H. (College of Aeronautics, )

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- Craven, A. H. (10)
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- Hopkins, H. L. (1)