Fall 2013 AAE 251: Introduction to Aerospace Design
Homework Assignment # 3
Electronic Handout: 13 September 2013
Due: 20 September 2013
Be sure to use appropriate units. Show all of the important steps in your solution. Box your nal answers.
Be sure to f

Fall 2013 AAE 251: Introduction to Aerospace Design
Homework Assignment # 1
Electronic Handout: 27 August 2013
Due: 6 September 2013
Be sure to use appropriate units. Show all of the important steps in your solution. Box your nal answers.
Be sure to follo

Fall 2013 AAE 251: Introduction to Aerospace Design
Homework Assignment # 2
Electronic Handout: 6 September 2013
Due: 13 September 2013
Be sure to use appropriate units. Show all of the important steps in your solution. Box your nal answers.
Be sure to fo

AAE251 HW1 Solutions
2
Aircraft
AV8-B Harrier
F-22 Raptor
A-10 Thunderbolt
Wing Location
High
Mid
Low
Dihedral
Anhedral
Flat
Dihedral
Planform
Swept or Delta
Delta
Tapered
Sweep
Yes
Yes
No
3
A Matlab function to calculate the temperature, pressure, and de

AAE 251: Introduction to Aerospace Design
Spring 2013
Due Friday April 5th
1. A Russian satellite is in Earth orbit with an altitude at perigee of 375 km and an altitude at
apogee of 2000 km
a) What is the semimajor axis of the orbit?
b) What is the eccen

Fall 2016 AAE 251: Introduction to Aerospace Design
Assignment #2: The Standard Atmosphere
Expected completion date: 30 August 2016
Be sure to use appropriate units. Show all of the important steps in your solution. Box your final answers.
Be sure to foll

Fall 2016 AAE 251: Introduction to Aerospace Design
Homework Assignment # 3
Expected completion date: 1 September 2016
Be sure to use appropriate units. Show all of the important steps in your solution. Box your final answers.
Be sure to follow all submis

AAE 251: Introduction to Aerospace Design
How Thrust is Made
9.8 Consider a rocket engine in which the combustion chamber pressure and temperature are 30
atm and 3756 K, respectively. The area of the rocket nozzle exit is 15 m2 and is designed so that
the

Name
Solution
Team Number
AAE 251: Introduction to Aerospace Design
Assignment 5Lift and Drag
Due Tuesday 1 March
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate boxes.
1
Question 1
You managed to survi

clear all
close all
clc
% Problem 1
%a) Plot of the lift and drag coefficients
% Create a vector "M" to span the range of Mach numbers of interest
M
= 1.2:0.01:2.5;
% Init

AIAA 2011-3505
29th AIAA Applied Aerodynamics Conference
27 - 30 June 2011, Honolulu, Hawaii
Drogue Parachute Effects on the Orion Crew Module
Stability
Downloaded by PURDUE UNIVERSITY on September 23, 2013 | http:/arc.aiaa.org | DOI: 10.2514/6.2011-3505

Fall 2013 AAE 251: Introduction to Aerospace Design
Homework Assignment # 6 - Airport Tour and Stability Concepts
Electronic Handout: 27 September 2013
Due: 11 October 2013
Be sure to use appropriate units. Show all of the important steps in your solution

Fall 2013 AAE 251: Introduction to Aerospace Design
Homework Assignment # 5
Electronic Handout: 25 September 2013
Due: 30 September 2013
Be sure to use appropriate units. Show all of the important steps in your solution. Box your nal answers.
Be sure to f

Fall 2016 AAE 251: Introduction to Aerospace Design
Homework Assignment # 7
Expected completion date: 13 September 2016
Be sure to use appropriate units. Show all of the important steps in your solution. Box your final answers.
Be sure to follow all submi

Fall 2016 AAE 251: Introduction to Aerospace Design
Homework Assignment # 6
Expected completion date: 11 September 2016
Be sure to use appropriate units. Show all of the important steps in your solution. Box your final answers.
Be sure to follow all submi

Name
Team Number
SOLUTION
AAE 251: Introduction to Aerospace Design
Assignment 6The Rocket Equation, Rocket Thrust and
Staging
Due Tuesday 8 March
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate boxes.

Name: Solutions
Team:
AAE251 Spring 2016 Quiz 2
Prof. Karen Marais
Maximum score = 60
Time: 5 minutes reading + 70 minutes
You may not leave in the last ten minutes of the exam.
Do not turn the page until told do so.
Closed book and closed notes.
For your

Name
Solutions
Team Number
AAE 251: Introduction to Aerospace Design
Assignment 8Aircraft Performance I
Due Tuesday April 5
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate boxes.
1
Question 1
Many aircr

Name
Team Number
Solution
AAE 251: Introduction to Aerospace Design
Assignment 3Orbits and Launch to LEO
Due Tuesday 9 February
Instructions
This assignment has six problemsthree each for the lectures, Intro to Orbits, and
Launch to LEO. The questions are

Name
Solution
Team Number
AAE 251: Introduction to Aerospace Design
Assignment 4Aircraft Sizing and Lift and Drag
Due Tuesday 23 February
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate boxes.
1
Problem

Name:
Team:
AAE251 Spring 2015 Quiz 1
Prof. Karen Marais
Maximum score = 60
Time: 5 minutes reading + 70 minutes
You may not leave in the last ten minutes of the exam.
Do not turn the page until told do so.
Closed book and closed notes.
For your own benef

Name
Team Number
Solutions
AAE 251: Introduction to Aerospace Design
Assignment 9 Aircraft Performance II
Due Tuesday April 12
Instructions
Print the assignment out single-sided. Write or paste your answers into the appropriate boxes.
Please note that to

Name
Team Number
Solution
AAE 251: Introduction to Aerospace Design
Assignment 2Subsonic Wind Tunnels and the Space
Environment
Due Tuesday 2 February
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate box

Name:
Team:
AAE251 Spring 2016 Quiz 3
Prof. Karen Marais
Maximum score = 60
Time: 5 minutes reading + 70 minutes
You may not leave in the last ten minutes of the exam.
Do not turn the page until told do so.
Closed book and closed notes.
For your own benef

Name
Team Number
Solution
AAE 251: Introduction to Aerospace Design
Assignment 1Pitot Tubes
Due Tuesday 26 January
Instructions
This assignment has two partsthe derivation and application of Pitot tubes, and a
Matlab assignment. Start now, or you will run

Name
Team Number
SOLUTION
AAE 251: Introduction to Aerospace Design
Assignment 7Rocket Design I and II
Due Tuesday 29 March
Instructions
Print the assignment out single-sided. Write or paste your answers into the
appropriate boxes. Please note that to ans