An experimental and computational investigation of an annular reverse-flow combustor

The Performance of 60º Delta Wings: The Effects of Leading Edge Radius on Vortex Flaps and the Wing

Starting in 1946 as the College of Aeronautics, the Cranfield Institute of Technology was granted university status in 1969. In 1993 it changed its name to Cranfield University.

The Performance of 60º Delta Wings: The Effects of Leading Edge Radius and Vortex Flaps

Low-speed wind tunnel tests were conducted on sharp edge flat 60º delta wing, the wing with leading edge vortex flap deflected 30º and 60º delta wing with well rounded leading edge to estimate the effects of leading edge vortex flap and leading edge radius on the aerodynamic performance of 60º delta wings. Results indicate that the leading edge...

Tabular and graphical solutions of regular and mach reflections in pseudo-stationary frozen and vibrational-equilibrium flows. Part 1.

Tabular and graphical solutions of regular mach reflections in speudo-stationary frozen and vibrational-equilibrium flows. Part 2.

Pseudo-stationary oblique-shock-wave reflections in a polyatomic gas-sulfur hexafluoride

The influence of fresnel number and geometric parameters on the diffracted field of planar lamina