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A nacelle configured to be coupled to an underside of a wing so as to form a clearance space therebetween includes at least a lip defining an inlet and a first cowling disposed aft of the lip. The first cowling has an outer surface with at least one concave region that is depressed relative to anoth

A nacelle configured to be coupled to an underside of a wing so as to form a clearance space therebetween includes at least a lip defining an inlet and a first cowling disposed aft of the lip. The first cowling has an outer surface with at least one concave region that is depressed relative to another region of the outer surface. In some aspects, the depressed region can be disposed on an inboard side of the wing, for example, on an upper surface of the first cowling facing a wing. The nacelle can include a second cowling disposed between the lip and the first cowling and the first cowling can translate in a longitudinal direction relative to the second cowling.

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1. A nacelle having a longitudinal axis and being configured to be coupled by a pylon to an underside of a wing having a swept wing configuration, the wing having a leading edge, the nacelle comprising: a lip defining an inlet; anda first cowling disposed aft of the lip and at least partially inboar

1. A nacelle having a longitudinal axis and being configured to be coupled by a pylon to an underside of a wing having a swept wing configuration, the wing having a leading edge, the nacelle comprising: a lip defining an inlet; anda first cowling disposed aft of the lip and at least partially inboard of the pylon, the first cowling having a non-undulating trailing edge and an outer surface including a critical surface region localized between the wing and an inboard side of an upper surface of the nacelle to define an inboard flow area between the nacelle and the underside of the wing, the outer surface including a depression isolated at least one of near or in the critical surface region thereof, the depression being recessed relative to an adjacent portion of the outer surface and extending forward of the leading edge of the wing to an outlet of the nacelle. 2. The nacelle of claim 1, wherein the depression includes a curvature having a slope that is at least partially directed toward a centerline of the nacelle. 3. The nacelle of claim 1, wherein a transverse distance between the outer surface of the first cowling and the longitudinal axis of the nacelle is greater than a transverse distance between the depression and the longitudinal axis. 4. A nacelle having a longitudinal axis and being configured to be coupled by a pylon to an underside of a wing, the nacelle and a leading edge of the wing defining a first flow area on an inboard side of the pylon and a second flow area on an outboard side of the pylon the second flow area being greater than the first flow area, the nacelle comprising: a lip defining an inlet; anda first cowling having an outer surface, the outer surface defining a contour extending forward of the leading edge of the wing to an outlet of the nacelle, the contour having only two points of inflection defining at least in part a single depression isolated at least one of near or in a critical surface region of the outer surface, and defining a portion of the first flow area and extending forward of the leading edge of the wing to an outlet of the nacelle, the critical surface region localized between the wing and the inboard side of the upper surface of the nacelle and the contour configured to reduce compression of fluid flow along the leading edge of the wing. 5. The nacelle of claim 4, wherein the depression has a concave shape. 6. The nacelle of claim 5, wherein the depression is disposed aft of the lip. 7. The nacelle of claim 4, wherein the outer surface comprises a first radius of curvature defined between the longitudinal axis and a portion of the outer surface that is disposed on an inboard side of the nacelle and a second radius of curvature defined between the longitudinal axis and a portion of the outer surface that is disposed on an outboard side of the nacelle, the first radius of curvature being less than the second radius of curvature. 8. The nacelle of claim 4 further comprising a second cowling disposed between the lip and the first cowling. 9. The nacelle of claim 8, wherein the first cowling is configured to translate along the longitudinal axis relative to the second cowling. 10. A nacelle having a longitudinal axis, comprising: a lip defining an inlet;a translating sleeve at least partially defining a non-undulating outlet and being configured to translate in a longitudinal direction relative to the lip between at least a first configuration and a second configuration, the translating sleeve having an surface which is configured to face an underside of a wing, the upper surface including a depression aft a forward pylon attachment point inboard of a pylon, the depression defined from forward of a leading edge of the wing to an outlet of the nacelle and disposed below the underside of the wing and configured to increase a flow area and reduce fluid compression on a portion of the leading edge of the wing inboard the pylon; anda cascade having at least a first portion disposed between the translating sleeve and the longitudinal axis when the translating sleeve is in the first configuration, the first portion of the cascade being exposed when the translating sleeve is in the second configuration. 11. The nacelle of claim 10, wherein the first portion of the cascade comprises a plurality of vanes. 12. The nacelle of claim 10, wherein a second portion of the cascade is disposed between the depression and the longitudinal axis when the translating sleeve is in the first configuration. 13. The nacelle of claim 12, wherein the second portion of the cascade does not comprise any vanes. 14. The nacelle of claim 10 further comprising a plurality of blocker doors configured to be activated to at least partially impinge an air pathway defined between the inlet and an outlet of the nacelle at least when the translating sleeve is in the second configuration. 15. The nacelle of claim 14, wherein the plurality of blocker doors at least partially define a channel extending between the inlet and the outlet of the nacelle when the blocker doors are activated, at least a portion of the channel being, disposed between the depression and the longitudinal axis of the nacelle.