EMBRY-RIDDLE AERONAUTICAL UNIVERSITY
Daytona Beach Campus
AE 413: Aircraft Stability and Control
Instructor: Claudia Moreno, Ph.D
Fall 2014
HOMEWORK #1
Due Date: September 4, 2015
1. The Cessna T-37 is a small military trainer aircraft that ew for decades

AE 302
Aerodynamics II
Fall 2015
Homework 3 (due 09/24/15 in class, as it starts)
1.
2.
3.
4.
5.
6.
Problem 5.11 in Anderson, " Aircraft Performance "
Problem 5.12 in Anderson, " Aircraft Performance "
Problem 5.14 in Anderson, " Aircraft Performanc

AE 302
Aerodynamics II
Fall 2015
Homework 2 (due 09/17/15 in class, as it starts)
1. Considering the aircraft described in Problem 5.1 in Anderson, " Aircraft Performance ",
calculate:
a) The maximum values of CL / CD, CL1/2 / CD, and CL3/2 / CD
b) The ve

AE 302
Aerodynamics II
Fall 2015
Homework 3 (due 09/24/15 in class, as it starts)
1.
2.
3.
4.
5.
6.
Problem 5.11 in Anderson, " Aircraft Performance "
Problem 5.12 in Anderson, " Aircraft Performance "
Problem 5.14 in Anderson, " Aircraft Performanc

AE 302
Aerodynamics II
Fall 2015
Homework 2 (due 09/17/15 in class, as it starts)
1. Considering the aircraft described in Problem 5.1 in Anderson, " Aircraft Performance ",
calculate:
a) The maximum values of CL / CD, CL1/2 / CD, and CL3/2 / CD
b) The ve

EMBRY-RIDDLE AERONAUTICAL UNIVERSITY
Daytona Beach Campus
AE 413: Aircraft Stability and Control
Instructor: Dr. Claudia Moreno
Fall 2015
HOMEWORK #3
Due Date: October 7, 2015
1. (40 points) In this problem we will continue with the calculation of longitu

EMBRY-RIDDLE AERONAUTICAL UNIVERSITY
Daytona Beach Campus
AE 413: Aircraft Stability and Control
Instructor: Dr. Claudia Moreno
Fall 2015
HOMEWORK #2
Due Date: September 25, 2015
1. (10 points) Do problem 2.10 in your text book.
2. (20 points) This proble

AE 302
Aerodynamics II
Fall 2015
Homework 5 (due 10/22/15 in class, as it starts)
1/3
2/3
5. Problem 8.12 in Anderson, " Fundamentals of Aerodynamics "
3/3

AE 302
Aerodynamics II
Fall 2015
Homework 4 (due 10/20/15 in class, as it starts)
Unless specified otherwise, assume the working fluid is air and it can be treated as an ideal
gas with constant specific heats. The specific gas constant for air is:
! = 287

AE 302
Aerodynamics II
Fall 2015
Homework 1 (due 09/10/15 in class, as it starts)
1.
The of efficiency of a propeller for the range of advance ratio 1 < J < 2.5 is given by the
following empirical relation
2
J 2 2
r
pr = 0.8 ( J 4r*)
, 0.2 r* = 1
R