Nacelle

1. A nacelle encircling an engine about an axis of rotation, comprising:

an inlet cowling defining an inlet of the nacelle, wherein the inlet cowling comprises an inlet cowling outer surface defining an outermost circumferential surface of the inlet cowling and an inlet cowling aft edge spanning radially inward from the inlet cowling outer surface, wherein the inlet cowling aft edge comprises an aft edge length and an aft edge outer point which is the radially outermost point of the inlet cowling aft edge; and

a boat tail cowling disposed aft of the inlet cowling, wherein the boat tail cowling comprises a boat tail cowling outer surface defining an outermost circumferential surface of the boat tail cowling, and a boat tail cowling forward edge spanning radially inward from the boat tail cowling outer surface, wherein the boat tail cowling forward edge comprises a forward edge length and a forward edge outer point which is the radially outermost point of the boat tail cowling forward edge, wherein the boat tail cowling forward edge is disposed adjacent to and abutting the inlet cowling aft edge,

wherein the aft edge outer point of the inlet cowling aft edge is more radially outward than the forward edge outer point of the boat tail cowling forward edge, forming a step, the step being defined by a portion of the inlet cowling aft edge that is radially further outward than the forward edge outer point of the boat tail cowling forward edge.

2. The nacelle of claim 1 , wherein the step is disposed aft of an inlet cowling maximum point.

3. The nacelle of claim 1 , further comprising a thrust reverser coupled to the inlet cowling and the boat tail cowling, wherein the boat tail cowling is configured to translate in an aft direction, wherein the boat tail cowling forward edge is disposed adjacent to and abutting the inlet cowling aft edge when the boat tail cowling is in a forward-most configuration, and wherein the thrust reverser is configured to be in an exposed configuration in response to the boat tail cowling translating in the aft direction.

4. The nacelle of claim 3 , wherein the step is disposed forward of the thrust reverser in the exposed configuration.

5. The nacelle of claim 1 , wherein the aft edge outer point is at an inlet cowing maximum point.

6. The nacelle of claim 1 , wherein the aft edge outer point is aft of an inlet cowling maximum point.

7. The nacelle of claim 6 , wherein the inlet cowling comprises a convergent surface between the inlet cowling maximum point and the aft edge outer point.

8. The nacelle of claim 7 , where in the convergent surface is flat.

9. The nacelle of claim 7 , wherein the convergent surface is at least one of convex or concave.

10. The nacelle of claim 7 , wherein a convergent angle formed between the convergent surface and a reference line parallel to the axis of rotation is between 0.01 and 18 degrees.

11. The nacelle of claim 1 , wherein at least a portion of the inlet cowling aft edge comprises an angled portion.

12. The nacelle of claim 11 , wherein an angle formed between the angled portion and a reference line parallel to the axis of rotation is between 45 and 90 degrees.

13. An aircraft, comprising:

a gas turbine engine; and

a nacelle encircling the gas turbine engine, comprising:

an inlet cowling defining an inlet of the nacelle, wherein the inlet cowling comprises an inlet cowling outer surface defining an outermost circumferential surface of the inlet cowling and an inlet cowling aft edge spanning radially inward from the inlet cowling outer surface, wherein the inlet cowling aft edge comprises an aft edge length and an aft edge outer point which is the radially outermost point of the inlet cowling aft edge; and

a boat tail cowling disposed aft of the inlet cowling, wherein the boat tail cowling comprises a boat tail cowling outer surface defining an outermost circumferential surface of the boat tail cowling, and a boat tail cowling forward edge spanning radially inward from the boat tail cowling outer surface, wherein the boat tail cowling forward edge comprises a forward edge length and a forward edge outer point which is the radially outermost point of the boat tail cowling forward edge, wherein the boat tail cowling forward edge is disposed adjacent to and abutting the inlet cowling aft edge,

wherein the aft edge outer point of the inlet cowling aft edge is more radially outward than the forward edge outer point of the boat tail cowling forward edge, forming a step, the step being defined by a portion of the inlet cowling aft edge that is radially further outward than the forward edge outer point of the boat tail cowling forward edge.

14. The aircraft of claim 13 , wherein the step is disposed aft of an inlet cowling maximum point.

15. The aircraft of claim 13 , further comprising a thrust reverser coupled to the inlet cowling and the boat tail cowling, wherein the boat tail cowling is configured to translate in an aft direction, wherein the boat tail cowling forward edge is disposed adjacent to and abutting the inlet cowling aft edge when the boat tail cowling is in a forward-most configuration, wherein the thrust reverser is configured to be in an exposed configuration in response to the boat tail cowling translating in the aft direction, and wherein the step is disposed forward of the thrust reverser in the exposed configuration.

16. The aircraft of claim 13 , wherein the aft edge outer point is aft of an inlet cowling maximum point.

17. The aircraft of claim 16 , wherein the inlet cowling comprises a convergent surface between the inlet cowling maximum point and the aft edge outer point.

18. The aircraft of claim 17 , wherein a convergent angle formed between the convergent surface and a reference line parallel to the axis of rotation is between 0.01 and 18 degrees.

19. The aircraft of claim 13 , wherein at least a portion of the inlet cowling aft edge comprises an angled portion.