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 a radially outermost point of the inlet cowling aft edge;

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 a radially outermost point of the boat tail cowling forward edge, and 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; and

a transition fairing coupled to and radially outward of the boat tail cowling outer surface of the boat tail cowling, wherein the transition fairing and the boat tail cowling are separate components coupled together, wherein the transition fairing comprises: a fairing forward edge spanning radially outward from the boat tail cowling outer surface and disposed adjacent to the inlet cowling aft edge; and a fairing ramp surface providing a transition surface between the inlet cowling aft edge and the boat tail cowling outer surface, wherein there is a discontinuity between the fairing ramp surface and the boat tail cowling outer surface.

2. The nacelle of claim 1 , wherein the aft edge outer point is radially further outward than a radially outermost point of the fairing forward edge.

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 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.

4. The nacelle of claim 3 , wherein the step is disposed forward of the thrust reverser and the transition fairing is disposed radially outward of the thrust reverser.

5. The nacelle of claim 1 , wherein the inlet cowling comprises a convergent surface between an inlet cowling maximum point and the aft edge outer point of the inlet cowling aft edge.

6. The nacelle of claim 5 , wherein the fairing ramp surface spans between the boat tail cowling outer surface and the aft edge outer point.

7. The nacelle of claim 6 , wherein the convergent surface and the fairing ramp surface are flush.

8. The nacelle of claim 5 , wherein the fairing ramp surface spans between the boat tail cowling outer surface and a point along the inlet cowling aft edge that is radially inward of the aft edge outer point.

9. The nacelle of claim 1 , wherein a transition angle formed between the fairing ramp surface and a reference line parallel to the axis of rotation is between 10 and 20 degrees.

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

11. 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 a radially outermost point of the inlet cowling aft edge;

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 a 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; and

a transition fairing coupled to and radially outward of the boat tail cowling outer surface of the boat tail cowling, wherein the transition fairing and the boat tail cowling are separate components coupled together, wherein the transition fairing comprises: a fairing forward edge spanning radially outward from the boat tail cowling outer surface and disposed adjacent to the inlet cowling aft edge; and

a fairing ramp surface providing a transition surface between the inlet cowling aft edge and the boat tail cowling outer surface, wherein there is a discontinuity between the fairing ramp surface and the boat tail cowling outer surface.

12. The aircraft of claim 11 , wherein the aft edge outer point is radially further outward than a radially outermost point of the fairing forward edge.

13. The aircraft of claim 11 , 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 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.

14. The aircraft of claim 13 , wherein the step is disposed forward of the thrust reverser, and the transition fairing is disposed radially outward of the thrust reverser.

15. The aircraft of claim 11 , wherein the inlet cowling comprises a convergent surface between an inlet cowling maximum point and the aft edge outer point of the inlet cowling aft edge.

16. The aircraft of claim 15 , wherein the fairing ramp surface spans between the boat tail cowling outer surface and the aft edge outer point.

17. The aircraft of claim 15 , wherein the fairing ramp surface spans between the boat tail cowling outer surface and a point along the inlet cowling aft edge that is radially inward of the aft edge outer point.

18. The aircraft of claim 11 , wherein a transition angle formed between the fairing ramp surface and a reference line parallel to an axis of rotation is between 10 and 20 degrees.