Similarity solution for a laminar, incompressible jet flowing along a curved surface.
Similarity transformation and perturbation solution for laminar two dimensional incompressible jet flow over curved surface of small curvature
Greber, I.↗
Engineering topics
Greber, I.
Publications and source records attributed to Greber, I..
Experimental scaling study of fluid amplifier elements
Study examines scaling parameters of three fluid amplifier elements - a bistable device, a boundary layer control device, and a vortex device. Variations in performance due to size, fluid, and other conditions are studied. Even with restricted examples the large number of variables impedes the establishment of these scaling laws.
Abler, J.↗
Similarity solution of a jet flowing over a curved surface
Similarity solution of laminar two-dimensional incompressible jet flowing over curved surface
LAMINAR JET↗
Experimental scaling study of fluid amplifier elements Final report
Scaling parameters of three fluid amplifier elements - bistable, boundary layer control, and vortex devices
BOUNDARY LAYER CONTROL↗
The Interaction of an Oblique Shock Wave with a Laminar Boundary Layer
The results of some experimental and theoretical studies of the interaction of oblique shock waves with laminar boundary layers are presented. Detailed measurements of pressure distribution, shear distribution, and velocity profiles were made during the interaction of oblique shock waves with laminar boundary layers on a flat plate. From these measurements a model was derived to predict the pressure levels characteristic of separation and the length of the separated region.
Hakkinen, R. J.↗