Module Details |
The information contained in this module specification was correct at the time of publication but may be subject to change, either during the session because of unforeseen circumstances, or following review of the module at the end of the session. Queries about the module should be directed to the member of staff with responsibility for the module. |
Title | AERODYNAMICS | ||
Code | AERO316 | ||
Coordinator |
Dr S Timme Mechanical, Materials & Aerospace Eng Sebastian.Timme@liverpool.ac.uk |
||
Year | CATS Level | Semester | CATS Value |
Session 2017-18 | Level 6 FHEQ | First Semester | 15 |
Aims |
|
The module aims to help the student to develop the ability to understand qualitatively and to predict quantitatively the flow over an aerofoil at all speeds, and the flow over simple wings. |
Learning Outcomes |
|
On successful completion of the module the students will be able to apply the appropriate aerodynamic theory depending on the flow conditions and assess the limitations of the data with reference to the limitations of the methods applied. | |
On successful completion of the module the students will be able to analyse aerofoils for their aerodynamic characteristics. |
|
On successful completion of the module the students will be able analyse simple wings for their aerodynamic characteristics |
|
On successful completion of the module the students should have strengthened reporting skills and use the accepted technical language accordingly. |
Syllabus |
|
1 |
Flow Modelling and Conservation Laws - Navier-Stokes equations, Euler equations, Laplace equation, Aerodynamic Hierarchy
Potential Flow Theory - Laplace equation, velocity potential function, stream function, vorticity, Bernoulli''s equation, irrotational flow, circulation Thin Aerofoil Theory - circulation theory of lift, lift, drag and moments on aerofoils, aerodynamic centre, centre of pressure, compressibility correction Shock/Expansion Theory - oblique shock wave, Prandtl-Meyer expansion Boundary Layers - separation, pressure g radients, laminar and turbulent. Lifting Line Theory - flow over finite wings |
Teaching and Learning Strategies |
|
Lecture - Lectures to introduce and explain the material, classroom exercises Lecture notes are uploaded to Vital |
|
Laboratory Work - Computer exercises using MATLAB and XFOIL Handouts uploaded to Vital |
Teaching Schedule |
Lectures | Seminars | Tutorials | Lab Practicals | Fieldwork Placement | Other | TOTAL | |
Study Hours |
48 Lectures to introduce and explain the material, classroom exercises |
6 Computer exercises using MATLAB and XFOIL |
54 | ||||
Timetable (if known) |
Lecture notes are uploaded to Vital
|
Handouts uploaded to Vital
|
|||||
Private Study | 96 | ||||||
TOTAL HOURS | 150 |
Assessment |
||||||
EXAM | Duration | Timing (Semester) |
% of final mark |
Resit/resubmission opportunity |
Penalty for late submission |
Notes |
Unseen Written Exam | 180 | Semester 1 | 100 | No reassessment opportunity | Standard UoL penalty applies | Written Exam There is no reassessment opportunity, year 3 module Notes (applying to all assessments) - none |
CONTINUOUS | Duration | Timing (Semester) |
% of final mark |
Resit/resubmission opportunity |
Penalty for late submission |
Notes |
Recommended Texts |
|
Reading lists are managed at readinglists.liverpool.ac.uk. Click here to access the reading lists for this module. Explanation of Reading List: |