A theory for slender delta wings with leading edge blowing

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

On the application of boundary layer control to a slender wing supersonic airliner cruising at M = 2.2

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

The compressible laminar boundary layer with foreign gas injection

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

Base Pressure at Supersonic Speeds in the Presence of a Supersonic Jet

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

Boundary Layers with Suction and Injection: A review of published work on skin friction

Available data on the effects of suction and injection on skin friction are summarised and compared. It is shown that injection into a turbulent boundary layer can produce a skin friction coefficient lower than the laminar value at the same Reynolds number on an impermeable plate. The College of Aeronautics was founded in 1946 and was granted...

Base pressure at subsonic speeds in the presence of a supersonic jet

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

The aerodynamic derivates of an aerofoil oscillating in an infinite staggered cascade

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

The Effect of Density on Jet Flow at Subsonic Speeds

On the assumption that the velocity and density distributions across a jet of one gas issuing into a stream of a second gas are of exponential form, the momentum integral approach has been employed to find the variation of centre-line velocity downstream of the potential core. The results for the particular case of a jet issuing into a gas at...

Effect of body incidence on two afterbodies with a rearward facing jet

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

Interference of a rearward facing jet on the flow over three representative afterbody shapes in a uniform subsonic flow

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

The free streamline method applied to the flow at the rear of a duct

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

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

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.

The flexure-torsion flutter of cambered aerosoils in cascade

The College of Aeronautics was founded in 1946 and was granted university status in 1969 becoming the Cranfield Institute of Technology. In 1993 it changed its name to Cranfield University.