Author Information

Seshan JayapregashamFollow

Is this project an undergraduate, graduate, or faculty project?

Undergraduate

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What campus are you from?

Daytona Beach

Authors' Class Standing

Seshan Jayapregasham, Junior

Lead Presenter's Name

Seshan Jayapregasham

Faculty Mentor Name

Keshav Acharya

Abstract

Wind fields directly affect the performance of an aircraft in flight. With advancements in meteorology, air patterns and wind fields can be more accurately predicted. Through an understanding of how the behavior of these wind fields change the time needed to travel a set flight path, the duration of a set flight path can be shortened. In this presentation, I discuss the flight of an aircraft in an irrotational wind field. This study analyzes the effect of non-uniform linear wind speed on a flight in a closed-loop as a representation of a point moving in a vector field. Using previously established simplifications and representations of this situation in a fixed wind field, the basis of the study is expanded to irrotational wind fields of changing magnitude. This concept is also applied to other representations including turbine blades.

Did this research project receive funding support from the Office of Undergraduate Research.

Yes, SURF

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Flight in Irrotational Wind Field

Wind fields directly affect the performance of an aircraft in flight. With advancements in meteorology, air patterns and wind fields can be more accurately predicted. Through an understanding of how the behavior of these wind fields change the time needed to travel a set flight path, the duration of a set flight path can be shortened. In this presentation, I discuss the flight of an aircraft in an irrotational wind field. This study analyzes the effect of non-uniform linear wind speed on a flight in a closed-loop as a representation of a point moving in a vector field. Using previously established simplifications and representations of this situation in a fixed wind field, the basis of the study is expanded to irrotational wind fields of changing magnitude. This concept is also applied to other representations including turbine blades.

 

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