Passive jet system arranged at front wheels of a vehicle
A passive jet system for disrupting an airflow at a surface of a front wheel for a vehicle includes a duct including an inlet exposed to an airflow, an outlet fluidically directed toward a forward surface of the front wheel, and a passage having a flow-accelerating profile operable to increase a velocity of the airflow passing from the inlet toward the outlet.
1 . A passive jet system for disrupting an airflow at a surface of a front wheel for a vehicle, the passive jet system comprising
a duct including an inlet exposed to an airflow, an outlet fluidically directed directly onto a forward surface of the front wheel, and a passage having a flow-accelerating profile operable to increase a velocity of the airflow passing from the inlet toward the outlet,
wherein the duct includes a first member having a first end, a second end, and an intermediate portion having a first inner surface and a second member having a first end portion, a second end portion and an intermediate section having a second inner surface that is spaced from the first inner surface, at least one of the first inner surface and the second inner surface defining the flow-accelerating profile, and
wherein the second member includes an airfoil shaped cross-section.
2 . The passive jet system according to claim 1 , wherein the first end of the first member is arranged directly adjacent to the first end portion of the second member.
3 . The passive jet system according to claim 1 , wherein the first member includes a first lateral side and a second lateral side, and the second member includes a first lateral side portion and a second lateral side portion that are substantially parallel, the first lateral side being joined to the first lateral side portion by a first end plate and the second lateral side being joined to the second lateral side portion by a second end plate.
4 . The passive jet system according to claim 1 , wherein the inlet tapers from the first end toward the intermediate portion.
5 . The passive jet system according to claim 4 , wherein the inlet diverges from the first end toward the intermediate portion.
6 . The passive jet system according to claim 4 , wherein the inlet of the duct includes a first area and the outlet of the duct includes a second area, the second area being smaller than the first area.
7 . The passive jet system according to claim 1 , wherein the intermediate portion includes a first curvature and the intermediate section includes a second curvature that is distinct from the first curvature.
8 . The passive jet system according to claim 1 , wherein the inlet is axially off-set relative to the outlet.
9 . The passive jet system according to claim 1 , wherein the passage continuously increases in width from the inlet to the outlet.
10 . The passive jet system according to claim 1 , wherein the duct is configured to be mounted on an underbody of the vehicle.
11 . A vehicle comprising:
a body including a forwardly facing portion having a lower edge, a rearwardly facing portion and a passenger compartment positioned between the forwardly facing portion and the rearwardly facing portion;
a wheel well defined aft of the lower edge of the forwardly facing portion;
a wheel including a driving surface rotatably supported in the wheel well; and
a passive jet system mounted to the lower edge of the forwardly facing portion, the passive jet system including a duct having an inlet exposed to an airflow, an outlet fluidically directed directly onto the driving surface of the wheel, and a passage having a flow-accelerating profile operable to increase a velocity of the airflow passing from the inlet toward the outlet,
wherein the duct includes a first member having a first end, a second end, and an intermediate portion having a first inner surface and a second member having a first end portion, a second end portion and an intermediate section having a second inner surface that is spaced from the first inner surface, at least one of the first inner surface and the second inner surface defining the flow-accelerating profile, and
wherein the second member includes an airfoil shaped cross-section.
12 . The vehicle according to claim 11 , wherein the first end of the first member is arranged directly adjacent to the first end portion of the second member.
13 . The vehicle according to claim 11 , wherein the first member includes a first lateral side and a second lateral side, and the second member includes a first lateral side portion and a second lateral side portion that are substantially parallel, the first lateral side being joined to the first lateral side portion by a first end plate and the second lateral side being joined to the second lateral side portion by a second end plate.
14 . The vehicle according to claim 11 , wherein the inlet tapers from the first end toward the intermediate portion.
15 . The vehicle according to claim 14 , wherein the inlet diverges from the first end toward the intermediate portion.
16 . The vehicle according to claim 14 , wherein the inlet of the duct includes a first area and the outlet of the duct includes a second area, the second area being smaller than the first area.
17 . The vehicle according to claim 11 , wherein the intermediate portion includes a first curvature and the intermediate section includes a second curvature that is distinct from the first curvature.
18 . The vehicle according to claim 11 , wherein the inlet is axially off-set relative to the outlet.
19 . The vehicle according to claim 11 , wherein the passage continuously increases in width from the inlet to the outlet.
20 . The vehicle according to claim 11 , wherein the duct is mounted on an underbody of the vehicle.