EAE 127 - Applied Aircraft Aerodynamics

Fall 2009

 

Administrative Information

Textbook:

Aerodynamics Theoretical & Computational Fluid Dynamics For Engineers, Fifth Edition

John J. Bertin, Russell M. Cummings

Lectures:

Monday, Wednesday, Friday 11-11:50am

 

168 HOAGLAND

Discussion:

Friday 1:10-2:00pm

 

2016 HARING

 

syllabus.pdf (UPDATED 9/22/09)

 

Report Format and Grading

 

Sample Report

 

Contact Us

Instructor: Jean-Jacques Chattot

Phone No.:

530-752-0812

Office:

2004 Bainer Hall

Office Hours:

MWF 10-11 am, Bainer 2004

Email:

jjchattot@ucdavis.edu

Teaching Assistant: Kensuke Suzuki

Phone No.:

4-7578

Office:

112 TB 207

Office Hours:

W 9-10, R 11-12

Lab Hours:

R 2-3, F 9-10

Email:

kensuzuki@ucdavis.edu

 


Message: Project No. 7 is due Friday December 4.

 


Student Competitions:
FAA Airport Design Competition for Universities
AIAA Intelligent Systems Student Paper Competition
SAE Aero Design West Competition

 



Assignments

 

Projects are due at 5:00PM on the due date. They can be turned in at the MAE drop box C in front of Bainer 2015A

  •  Note: one way to save these files to disk is to right-click on them and choose “save target as”.

Help to compile a FORTRAN code in the CAE Lab

 



Resouces for Using C/C++ Interpreter

  • Download the C/C++ interpreter Ch Student or Professional Edition
  • Download ChSciTE IDE for Ch to run C/Ch/C++ Programs in Windows and Linux
  • Download Ch TextWrangler IDE to run C/Ch/C++ Programs in Mac OS X
  • Getting Started with ChSciTE Ch IDE to Run C/Ch/C++ Programs
  • Introduction to Ch
  • A Yahoo C/Ch/C++ User's Group to Ask Questions about Using C/Ch/C++
  • Feature Comparison of C/Ch/C++ with MATLAB and Mathematica
  • Syntax Comparison between Ch and MATLAB

  • Project 1 (Due Friday, 10/02  @5:00PM, In drop box C)

     


    Project 2 (Due Monday, 10/12  @5:00PM  In drop box C)

     


    Project 3 (Due Monday, 10/26  @5:00PM  In drop box C)

     


    Midterms

    Midterm Fall 2003  (midtermf03.pdf)

    Solution Midterm Fall 2003  (midtermsolf03.pdf)

    Midterm Fall 2004  (midtermf04.pdf)

    Solution Midterm Fall 2004  (midtermsolf04.pdf)

    Midterm Fall 2005  (midtermf05.pdf)

    Solution Midterm Fall 2005  (midtermsolf05.pdf)

    Midterm Fall 2006  (midtermf06.pdf)

    Solution Midterm Fall 2006  (midtermsolf06.pdf)

    Midterm Fall 2007  (midtermf07.pdf)

    Solution Midterm Fall 2007  (midtermsolf07.pdf)

    Midterm Fall 2008  (midtermf08.pdf)

    Solution Midterm Fall 2008  (midtermsolf08.pdf)

    Midterm Fall 2009  (midtermf09.pdf)

    Solution Midterm Fall 2009  (midtermsolf09.pdf)

     


    Project 4 (Due Monday, 11/09 @ 5:00PM in dropbox C) 

     


    Project 5 (due Monday, 11/16  @ 5:00PM In drop box C)

     


    Project 6 (Due Monday, 11/23  @ 5:00PM In drop box C)

     


    Project 7 (Due Friday, 12/04  @ 5:00PM In drop box C)

  • Project 7 Handout.doc
  • Notes on uaveq.f (PJ7-notes.txt)
  • Source Code (uaveq.f)
  • Input File (uaveq.data)
  • Executable (uaveq.exe)
  • S1707-0723 RE=0.3e6 POLAR (polars1707-0723)
  • Acceleration phase results (takeofftable.dat)
  • Source code (uaveq.ch)
  •  


    Sample Finals

    Final 2005

    Final Fall 2005  (final05.pdf)

    Solution Final Fall 2005  (finalsol05.pdf)

    Final 2006

    Final Fall 2006  (final06.pdf)

    Solution Final Fall 2006  (finalsol06.pdf)

    Final 2007

    Final Fall 2007  (final07.pdf)

    Solution Final Fall 2007  (finalsol07.pdf)

    Final 2008

    Final Fall 2008  (final08.pdf)

    Solution Final Fall 2008  (finalsol08.pdf)

     


     

    WINGLET PAPER – Paper published in the Journal of Aircraft. It studies the design of winglets, including viscous effects and looks at weathercock stability:

    Paper (C10725[001-005].pdf)