design-engine
New member
My Pro/CABLE work so far is nothing more than sculpture. Until I learn RSD I am a cable sculptor. Just a cool looking model.
The best part of Pro/E or 3d modeling that I think is addictive ... is the satisfaction of completing something so cool as a jet airplane or a mustang.... Years later when we look back at our models we realize mistakes or subtle differences. To learn Pro/E (or to get better like CPiotowski and I) we need something as engaging as a car or an airplane to keep the attention.
Look up boundary layer diverter in Wikipedia too
Boundary layer control apparatus is provided (22). The boundary layer
control apparatus (22) is for use with an aircraft propulsion nacelle
(12) positioned such that the air inlet (14) of the propulsion nacelle
is located proximate an aircraft surface (10), wherein a boundary layer
is established on the surface when the aircraft is propelled through an
atmosphere, causing air to flow over the surface. The boundary layer
control apparatus (22) includes a duct having an entrance (24)
positioned between the aircraft surface (10) and the inlet (14) of the
propulsion nacelle (12) for capturing the boundary layer air passing
over the aircraft surface and diverting the boundary layer air away
from the inlet.
The best part of Pro/E or 3d modeling that I think is addictive ... is the satisfaction of completing something so cool as a jet airplane or a mustang.... Years later when we look back at our models we realize mistakes or subtle differences. To learn Pro/E (or to get better like CPiotowski and I) we need something as engaging as a car or an airplane to keep the attention.
Look up boundary layer diverter in Wikipedia too
Boundary layer control apparatus is provided (22). The boundary layer
control apparatus (22) is for use with an aircraft propulsion nacelle
(12) positioned such that the air inlet (14) of the propulsion nacelle
is located proximate an aircraft surface (10), wherein a boundary layer
is established on the surface when the aircraft is propelled through an
atmosphere, causing air to flow over the surface. The boundary layer
control apparatus (22) includes a duct having an entrance (24)
positioned between the aircraft surface (10) and the inlet (14) of the
propulsion nacelle (12) for capturing the boundary layer air passing
over the aircraft surface and diverting the boundary layer air away
from the inlet.