Graduation Semester and Year
2016
Language
English
Document Type
Thesis
Degree Name
Master of Science in Aerospace Engineering
Department
Mechanical and Aerospace Engineering
First Advisor
Atilla Dogan
Abstract
The fuel saving benefit of formation flight has been demonstrated through theoretical and computational analyses, simulation, wind tunnel and flight tests. When an aircraft flies in a specific region in the wake of another aircraft, it experiences upwash, which results in reduced drag and thus reduced thrust requirement. One specific USAF mission that can potentially benefit from formation flight is coronet missions. In a coronet mission, fighter aircraft are escorted and refueled, as needed, by tanker aircraft over a long range. During the flight, the receiver aircraft fly in formation with the tanker but outside of the wake of the tanker except when they need refueling. In this thesis, the idea of flying the receivers at the sweet spot within the wake of the tanker is investigated. A high fidelity simulation has been developed that models the relative motion of multiple aircraft, aerodynamic coupling between the aircraft, and the effect of mass variation through fuel burn and fuel transfer. Various coronet missions for F-15C and F-15E aircraft escorted by a KC-135R have been simulated. The simulation results are used to quantify the benefit of flying at the sweet spot as compared to outside the wake in terms of the amount of fuel saved. The results show a significant amount of fuel savings for the whole fleet of KC-135R and multiple F-15C or F-15E when the F-15s fly at the sweet spot. The results also showed that the fighter aircraft can fly longer before refueling if it flies at the sweet spot. This implies that the number of refueling maneuvers and number of tanker aircraft involved in a coronet mission can potentially be reduced. The possibility of additional savings is explored by comparing several trimming methods, as well as tracking the sweet spot. The results show that the trimming method only has an insignificant effect on the fuel burn, however, tracking the sweet spot yields significant additional fuel savings.
Keywords
Flight control, Formation flight, Simulation, Sweet spot
Disciplines
Aerospace Engineering | Engineering | Mechanical Engineering
License
This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.
Recommended Citation
Kniffin, Christopher Allen, "FORMATION FLIGHT FOR FUEL SAVING IN CORONET MISSIONS OF KC-135R AND F-15C/E" (2016). Mechanical and Aerospace Engineering Theses. 692.
https://mavmatrix.uta.edu/mechaerospace_theses/692
Comments
Degree granted by The University of Texas at Arlington