Now showing items 1-4 of 4
A technique for direct measurement of skin friction in supersonic combustion flow
(Virginia Tech, 1992-11-15)
Experimental and numerical investigation of transonic turbine cascade flow
(Virginia Tech, 1992-12-05)
A comprehensive study of the flowfield through a two-dimensional cascade of the high pressure turbine blades of a jet engine is presented. The main interest is the measurement and prediction of the mass-averaged total ...
Experimental and computational investigation of helium injection into air at supersonic and hypersonic speeds
(Virginia Tech, 1992-06-05)
Experiments were performed with two different helium injector models at different injector transverse and yaw angles in order to determine the mixing rate and core penetration of the injectant and the flow field total ...