Now showing items 1-3 of 3
A study of the large-scale structure in a supersonic slot injected flow field
(Virginia Tech, 1988-06-15)
The use of hot-wire anemometry in studying supersonic slot injection into a supersonic flow
(Virginia Tech, 1988-02-05)
Tangential supersonic slot injection (M = 1.7) of air into a supersonic air stream (M = 2.91) was studied with a dual hot wire probe. This probe was used to simultaneously determine total temperature and mass flux. Mean ...
Viscous solutions for the Navier Stokes equations using an upwind finite volume technique
(Virginia Tech, 1988-05-05)
The process of enhancing an upwind finite volume, two-dimensional, thin layer Navier Stokes solver to achieve complete Navier Stokes solutions is described. The shear stress and heat flux contributions are identified and ...