Parts 2 and 3 of the Term project - the Aerodynamic model and flutter prediction using the k-
method. At the end of the lab, you should submit your symbolic or numerical solutions to these
questions (in a .pdf file), with the Matlab code attached either as an appendix or within the body of
the questions. The aerodynamic B and C matrices have components: BC=[BbbBtbBbtBtt]=[CbbCt
bCbtCtt] Symbolic expressions for the Bbb and Bbt are: BbbBbb=0sbLz(sy)4dy=0sb2L(sy)3dy 1.
Derive and write out similar symbolic expressions for the remaining terms in the B and C matrices
(Btb, Btt,Cbb,Cbt,Ctb and Ctt). Add these to the template MATLAB code. 2. Now use the code to
evaluate the B and C matrices. Write out the values of the B and C matrices for kref=0.1. 3. Now
construct Vg,Vw plots and determine the flutter velocity. Please add these plots to the PDF. What
is the flutter velocity? Note that in the k-method, an artificial damping g is analysed. This quantity
going positive indicates flutter..
Parts 2 and 3 of the Term project the Aerodynamic model an.pdf
1. Parts 2 and 3 of the Term project - the Aerodynamic model and flutter prediction using the k-
method. At the end of the lab, you should submit your symbolic or numerical solutions to these
questions (in a .pdf file), with the Matlab code attached either as an appendix or within the body of
the questions. The aerodynamic B and C matrices have components: BC=[BbbBtbBbtBtt]=[CbbCt
bCbtCtt] Symbolic expressions for the Bbb and Bbt are: BbbBbb=0sbLz(sy)4dy=0sb2L(sy)3dy 1.
Derive and write out similar symbolic expressions for the remaining terms in the B and C matrices
(Btb, Btt,Cbb,Cbt,Ctb and Ctt). Add these to the template MATLAB code. 2. Now use the code to
evaluate the B and C matrices. Write out the values of the B and C matrices for kref=0.1. 3. Now
construct Vg,Vw plots and determine the flutter velocity. Please add these plots to the PDF. What
is the flutter velocity? Note that in the k-method, an artificial damping g is analysed. This quantity
going positive indicates flutter.
![Parts 2 and 3 of the Term project - the Aerodynamic model and flutter prediction using the k-
method. At the end of the lab, you should submit your symbolic or numerical solutions to these
questions (in a .pdf file), with the Matlab code attached either as an appendix or within the body of
the questions. The aerodynamic B and C matrices have components: BC=[BbbBtbBbtBtt]=[CbbCt
bCbtCtt] Symbolic expressions for the Bbb and Bbt are: BbbBbb=0sbLz(sy)4dy=0sb2L(sy)3dy 1.
Derive and write out similar symbolic expressions for the remaining terms in the B and C matrices
(Btb, Btt,Cbb,Cbt,Ctb and Ctt). Add these to the template MATLAB code. 2. Now use the code to
evaluate the B and C matrices. Write out the values of the B and C matrices for kref=0.1. 3. Now
construct Vg,Vw plots and determine the flutter velocity. Please add these plots to the PDF. What
is the flutter velocity? Note that in the k-method, an artificial damping g is analysed. This quantity
going positive indicates flutter.](https://image.slidesharecdn.com/parts2and3ofthetermprojecttheaerodynamicmodelan-230322064102-834c323d/85/Parts-2-and-3-of-the-Term-project-the-Aerodynamic-model-an-pdf-1-320.jpg)
