AE 1350A: Introduction to Aerospace Engineering

Fall Semester 2008

 

Instructor:              Dr. Robert D. Braun

                                 robert.braun@ae.gatech.edu

                                 321-3 Knight Building

                                   

Class Schedule:      MW 10:05 – 10:55 am, Guggenheim 246

                                

Textbooks:              Required: Anderson, John D., Introduction to Flight, 6th edition, McGraw-Hill, 2008.

 

Instructor Office Hours:      MWF 2:05 – 2:55 pm

 

TA:                          Xin Zhang

                                 xaxtoo@gmail.com

 

TA Office Hours:   Tues 2-3 pm; Wed 3-4pm in Knight 306

        Thurs 4:30-5:30pm in Weber 215

                                                           

Course web site:     http://www.ae.gatech.edu/people/rbraun/classes/introAEF08/index.html

 

Prerequisites:         None     

 

Course Overview:

AE 1350 provides an introduction to the field of aerospace engineering through a discussion of basic principles, aerospace disciplines and aerospace systems. Course content includes a historical perspective followed by an introduction to fluid mechanics, applied aerodynamics, propulsion, airplane performance, stability, orbital motion, and launch vehicle performance. Guest speakers will discuss recent advances in aerospace systems.

 

There will be five homework sets. Each assignment will be due at the beginning of the lecture, one week from the date it is handed out. No late homework assignments will be accepted. The class midterm will cover historical background, fundamental concepts of fluid mechanics, applied aerodynamics, propulsion and airplane performance (Chapters 1-6 and the first half of Chapter 9 in the Anderson text). All class material will be covered in a comprehensive final during finals week. The final exam will cover Anderson Chapters 7, 8 and the remaining Chapter 9 material, as well as that material required for the midterm. Both the midterm and final exam employ a closed book, closed notes format. A team design project is required and a report describing this project is due on the final day of the semester. The team project requires design, development, construction and flight of a small launch vehicle. Aerodynamic, stability, and flight mechanics predictions will be compared to flight data. A final report of 15 pages or less, not including an appendix for the source code, is required. This report must be written in a professional manner, documenting the project scope, significance, analysis approach, results and verification. The report should follow the AIAA conference publication standards and format.

 

Course Materials:

            Aug 18                  Syllabus

            Aug 18                  Course overview

            Aug 18                  Aerospace company listing

            Sept 22                  Team project guidelines  (updated Nov 7)

            Nov 10                  Team project

 

            Aug 18                  Lecture 1

            Aug 20                  Lecture 2: Aeronautics history

            Aug 25                  Lecture 3: Astronautics history

            Aug 27                  Lecture 4: Gas properties and the standard atmosphere

            Sept 3                    Lecture 5: Fluid mechanics

            Sept 15                  Lecture 6: Airplane flight

            Sept 17                  Lecture 7: Airfoils and wings

            Sept 24                  Lecture 8: Propulsion

            Sept 29                  Lecture 9: Airplane performance

            Oct 20                   Lecture 10: Stability and control

            Oct 27                   Lecture 11: Launch vehicle performance

            Nov 10                  Lecture 12: Orbital mechanics

 

Homework Assignments:

 

            Sept 3                    Homework 1

            Sept 17                  Homework 2

            Sept 29                  Homework 3

            Nov 3                    Homework 4

            Nov 17                  Homework 5