Problem Set 3 - 09 Feb 2024-1
pdf
keyboard_arrow_up
School
University of Texas, Arlington *
*We aren’t endorsed by this school
Course
5302
Subject
Aerospace Engineering
Date
Feb 20, 2024
Type
Pages
4
Uploaded by SHANCKSSS
1 MAE 3306 –
Flight Performance & Stability Spring Semester 2024 Ian Maynard • NH 125A E
-Mail: ian.maynard@uta.edu HOMEWORK P
ROBLEM S
ET 3 D
ISTRIBUTED
: 09
F
EBRUARY 2024 D
UE DATE
: 19
F
EBRUARY 2024 Name: ID: Problem 1
Write a computer program that uses the vortex panel method that was [50%/100%] described in Sec. 1.6, and do the following: (1)
Compute
and plot
the C
p
vs x/
c
pressure distribution on a NACA 2412
airfoil. (2)
Generate a table
of the section lift coefficient 𝑪
̃
𝑳
, section leading edge pitching moment coefficient 𝑪
̃
?
?𝒆
, and the section quarter-chord pitching moment coefficient 𝑪
̃
?
𝒄/𝟒
as a function of angle of attack 𝜶
from
-12°
to 16°
in 2° increments. (3)
Plot
𝑪
̃
𝑳
and
𝑪
̃
?
𝒄/𝟒
as a function of angle of attack 𝜶
(4)
In one plot, plot 𝑪
̃
𝑳
vs
𝜶
using thin airfoil theory,
plot
𝑪
̃
𝑳
vs
𝜶
using the vortex panel method, and plot the experimental NACA 2412 𝑪
̃
𝑳
vs
𝜶
data from Fig. 1.6.6. Compare and discuss the results. Notes: •
Use 100 nodes with 99 panels. Verification Data: •
Using 100 nodes, at 𝛼 = 2
°, 𝐶
̃
𝐿
= 0.50247
, 𝐶
̃
𝑚
𝑙𝑒
= −0.18441
, and 𝐶
̃
𝑚
𝑐/4
=
−0.05887
•
If you are not matching with these results, set your number of nodes to 12 and check your code’s results with the following:
•
The A matrix for 12 nodes (note that python indexes start at 0, not 1):
2 •
Vector for solving for gamma (using 12 nodes): •
Gamma values (using 12 nodes): •
Summation vector for calculating Vx and Vy (using 12 nodes): This is a matrix of eleven (n-1) 2x1 matrices •
The upper surface Cp values (using 12 nodes): •
The lower surface Cp values (using 12 nodes): •
𝐶
̃
𝐿
summation vector (using 12 nodes):
3 •
𝐶
̃
𝑚
𝐿𝐸
summation vector (using 12 nodes): Problem 2
Using the thin airfoil theory code developed in homework 2 and the vortex [50%/100%] panel method code developed in problem one above, do the following:
(1)
Digitize the “
experimental data
”
points from Fig. 1.6.6 for the NACA 2412 using webplotdigitizer
. (2)
Recreate Fig. 1.6.6: In one plot, plot 𝑪
̃
𝑳
vs
𝜶
from -16°
to 16° in 2° increments
using (a) thin airfoil theory and
(b) the vortex panel method for a
NACA 2412 airfoil.
Also plot the experimental data for the
NACA 2412 airfoil. Discuss
the results. (3)
Digitize the “
experimental data
”
points from figure 1.6.7 for the NACA 2421 using webplotdigitizer
. (4)
Recreate Fig. 1.6.7: In one plot, plot 𝑪
̃
𝑳
vs
𝜶
from -16°
to 16° in 2° increments
using (a) thin airfoil theory and
(b) the vortex panel method for a
NACA 2421 airfoil.
Also plot the experimental data for the
NACA 2421 airfoil. Discuss
the results. (5)
Digitize the “
experimental data
”
points from figure 1.6.8 for the NACA 0015 using webplotdigitizer
. (6)
Recreate Fig. 1.6.8: In one plot, plot 𝑪
̃
𝑳
vs
𝜶
from -16°
to 16° in 2° increments
using (a) thin airfoil theory and
(b) the vortex panel method for a
NACA 0015 airfoil.
Also plot the experimental data for the
NACA 0015 airfoil. Discuss
the results. Notes: •
Use 100 nodes with 99 panels for the vortex panel method
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
- Access to all documents
- Unlimited textbook solutions
- 24/7 expert homework help
4 Homework General Requirements: »
Use MATLAB, Python, or another programming language to generate the answers and plots for all problems. »
Keep the programming codes neat and organized. »
Use professional plot formatting when generating plots. »
Include all the programming code that you have coded for your homework in your submission. Homework Formatting Requirements: »
Use engineering paper for all written solutions »
The header should include the student’s last name, then first name, class information (MAE 3306), homework number, date, and page number information »
Problem statement summaries are required (no need to rewrite entire problem statement if it is long, just summarize) »
List the inputs given, show all work in deriving the solution, and box or highlight
all final answers
. Plotted answers DO NOT need to be boxed. ---------- o0o ----------