Segmented landing gear door minimizes wake impingement on aerodynamic surfaces, reducing interaction noise by 2-5 dB.
A rotorcraft fairing features a truncated waterdrop profile with a transverse hump and relief projections to guide airflow.
Truncated flap support fairings employ active flow control nozzles to eject high velocity air, reducing drag and weight while avoiding engine exhaust heat.
Linear scale visualization of historical sensor readings reduces pilot observation time and cognitive workload during critical flight operations.
A shaft fairing with a 20 to 45 percent thickness ratio reduces aerodynamic drag by preventing flow separation around the interconnecting assembly.
Collapsible tape spring arms transition between contracted and extended states to position rotors radially outward from the main body.
Airfoil-shaped shaft fairing aligns wakes between upper and lower hubs to reduce aerodynamic drag on counter-rotating coaxial rotors.
A plate member mounted to a rotor shaft fairing increases the aspect ratio of the structure.