Abstract: An unmanned aerial vehicle including a frame elongated along a frame axis, the frame has a leading side and an aft side, the frame further includes a left end portion and a right end portion, a first forward rotor assembly connected to the left end portion of the frame, a second forward rotor assembly connected to the right end portion of the frame, the first forward rotor assembly and the second forward rotor assembly being positioned on the leading side of the frame, a compartment connected to the frame, the compartment having a leading side, and a curved leading-edge fairing disposed on the frame, wherein a portion of the curved leading-edge fairing extends to cover the leading side of the compartment, and wherein the curved leading-edge fairing reduces drag during flight in a forward direction to enable a substantially level flight profile.

Abstract: An unmanned aerial vehicle including a frame elongated along a frame axis, the frame has a leading side and an aft side, the frame further includes a left end portion and a right end portion, a first forward rotor assembly connected to the left end portion of the frame, a second forward rotor assembly connected to the right end portion of the frame, the first forward rotor assembly and the second forward rotor assembly being positioned on the leading side of the frame, a compartment connected to the frame, the compartment having a leading side, and a curved leading-edge fairing disposed on the frame, wherein a portion of the curved leading-edge fairing extends to cover the leading side of the compartment, and wherein the curved leading-edge fairing reduces drag during flight in a forward direction to enable a substantially level flight profile.

Abstract: An engine inlet air particulate separator that uses zero mass active flow control devices, and methods of using the same, are provided. The separator has a separator body that has an arcuate portion with a bight region. The separator body may have an angle ? between centerlines in the range from about 115° to about 85°. The separator body separates into a bypass conduit and a primary air conduit, separated from each other by a splitter, downstream from the bight region, which is in fluid communication with the arcuate portion. A zero mass active flow device is in fluid communication with a third region of the separator body which is located proximate a point where the air stream would otherwise have separated from an inner wall of the particle separator.