Apparatuses and methods for aerodynamic window assemblies

A method comprising:

• providing a windshield oriented toward a front of an aircraft, a side window oriented toward a side of the aircraft, and a post interposed between the windshield and the side window;
• and
• forming an airflow surface disposed on the post and on an exterior of the aircraft, the airflow surface extending along a length from a leading edge proximate the windshield to a trailing edge proximate the side window, the airflow surface extending along a height between a top and a bottom, the airflow surface having a first radius of curvature proximate the leading edge and a second radius of curvature proximate the trailing edge, wherein the first radius of curvature is less than the second radius of curvature.

An aerodynamic member configured to be secured to an aircraft window assembly, the aircraft window assembly comprising a windshield oriented toward a front of an aircraft, a side window oriented toward a side of the aircraft, and a post interposed between the windshield and the side window, the aerodynamic member comprising:

• an airflow surface configured to be disposed on the post and on an exterior of the aircraft when the aerodynamic member is secured to the aircraft window assembly, the airflow surface extending along a length from a leading edge of the airflow surface to a trailing edge of the airflow surface, the airflow surface extending along a height between a top and a bottom, the airflow surface having a first radius of curvature proximate the leading edge and a second radius of curvature proximate the trailing edge, wherein the first radius of curvature is less than the second radius of curvature.