| CPC B64C 3/28 (2013.01) [B64C 3/185 (2013.01); B64C 3/26 (2013.01); F16B 19/1045 (2013.01)] | 20 Claims |

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1. An aerodynamic structure, comprising:
a first skin region that includes a first skin edge;
a second skin region that includes a second skin edge, wherein the first skin region and the second skin region are angled relative to one another and define a gap between the first skin edge and the second skin edge;
a trailing edge structure that extends within the gap and between the first skin edge and the second skin edge, wherein the trailing edge structure includes:
(i) a leading region, which is positioned at least partially within the gap and includes a leading spar that defines a leading edge of the trailing edge structure and extends along a longitudinal length of the trailing edge structure, wherein the leading spar is a leading C-spar that is concave toward a trailing edge of the trailing edge structure, wherein a central curve of the leading C-spar defines the leading edge;
(ii) a trailing region, which defines the trailing edge; and
(iii) a transition region, which extends from the leading region to the trailing region; and
a plurality of blind fasteners, wherein:
(i) a first subset of the plurality of blind fasteners operatively interconnects the first skin region and the trailing edge structure; and
(ii) a second subset of the plurality of blind fasteners operatively interconnects the second skin region and the trailing edge structure;
wherein the first subset of the plurality of blind fasteners and the second subset of the plurality of blind fasteners both extend through a region of the trailing edge structure that is on a trailing side of the central curve of the leading C-spar; and
wherein the trailing edge structure is a monolithic trailing edge structure that defines an entirety of the leading region, the trailing region, and the transition region.
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