Question

3A) Explain in detail how the vortex panel/source panel method will solve the aerodynamics problems for arbitrary shape and thickness in order to calculate the aerodynamics characteristics. Students can explain through step by step procedures with the help of graphical illustration (4 Marks) 3B) By understanding the fundamental thin aerofoil theory for panel method (vortex or source panel method). Find one recent literatures on the research work that has been used these fundamental theory to solve the complex engineering problems especially in aerodynamics field.

          3A) Explain in detail how the vortex panel/source panel method will solve the
aerodynamics problems for arbitrary shape and thickness in order to calculate the
aerodynamics characteristics. Students can explain through step by step procedures with
the help of graphical illustration
(4 Marks)
3B) By understanding the fundamental thin aerofoil theory for panel method (vortex or
source panel method). Find one recent literatures on the research work that has been
used these fundamental theory to solve the complex engineering problems especially in
aerodynamics field.

3A) Explain in detail how the vortex panel/source panel method will solve the
aerodynamics problems for arbitrary shape and thickness in order to calculate the
aerodynamics characteristics. Students can explain through step by step procedures with
the help of graphical illustration
(4 Marks)
3B) By understanding the fundamental thin aerofoil theory for panel method (vortex or
source panel method). Find one recent literatures on the research work that has been
used these fundamental theory to solve the complex engineering problems especially in
aerodynamics field.

Added by Carlos H.

Question

Please give Ace some feedback