Hello, I am looking for someone to write an essay on The adaption of the Krmn vortex street phenomena to the application of multiple wingtip feathered winglets to the reductio. It needs to be at least

Hello, I am looking for someone to write an essay on The adaption of the Krmn vortex street phenomena to the application of multiple wingtip feathered winglets to the reductio. It needs to be at least 5750 words.

Thus, as a result, the overall shape and operating characteristics of aerospace vehicles resemble each other regardless of the company or the engineers which have worked on that particular design. Hence, similar characteristics pop up in each aerospace vehicle. However, there are many areas of improvement within these constrained design parameters. Especially as the fuel prices across the world soars every day, the concept of lowering the fuel cost for commercial, military as well as research vehicles have become more urgent then ever. Lowering the overall fuel consumption of the aerospace vehicle is an important criteria as it allows the aircraft to operate with less operational costs. Naturally, reduction in fuel consumption can be achieved by altering the various phases in the propulsion system of the aircraft. but the real reduction in fuel can only be achieved by lowering the aerodynamic drag that is acting upon the vehicle itself. This is quite important, as the overall drag force on the aerospace vehicle as well as the geometric zone of effect can have a large impact on the fuel consumption of the aero vehicle.