Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
With the continuous development of faster and cheaper computers of late, application of computational methods in solving engineering problems has become increasingly popular. New techniques are continuously being researched and developed in order to bring the numerical solution nearer to reality....
Saved in:
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | English English |
| Published: |
2004
|
| Subjects: | |
| Online Access: | http://psasir.upm.edu.my/id/eprint/263/1/549489_T_FK_2004_65.pdf |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| id |
my-upm-ir.263 |
|---|---|
| record_format |
uketd_dc |
| spelling |
my-upm-ir.2632013-05-27T06:47:05Z Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils 2004-06 Ahmad Yazid, Aznijar With the continuous development of faster and cheaper computers of late, application of computational methods in solving engineering problems has become increasingly popular. New techniques are continuously being researched and developed in order to bring the numerical solution nearer to reality. A Boundary Element Method is developed in the research to solve aerodynamic problems. Investigations revealed that the solution obtained using boundary element method is slightly superior to the solution provided by the currently used Panel Method. It was also found that the new technique also manages to obtain better result employing a lower number of nodes during solution, reducing the computational time. However, the adoption of potential theory means that the stall conditions of airfoils could still not be predicted at all. Boundary element methods Airfoils 2004-06 Thesis http://psasir.upm.edu.my/id/eprint/263/ http://psasir.upm.edu.my/id/eprint/263/1/549489_T_FK_2004_65.pdf application/pdf en public masters Universiti Putra Malaysia Boundary element methods Airfoils Faculty of Engineering English |
| institution |
Universiti Putra Malaysia |
| collection |
PSAS Institutional Repository |
| language |
English English |
| topic |
Boundary element methods Airfoils |
| spellingShingle |
Boundary element methods Airfoils Ahmad Yazid, Aznijar Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils |
| description |
With the continuous development of faster and cheaper computers of late, application of
computational methods in solving engineering problems has become increasingly
popular. New techniques are continuously being researched and developed in order to
bring the numerical solution nearer to reality. A Boundary Element Method is developed
in the research to solve aerodynamic problems. Investigations revealed that the solution
obtained using boundary element method is slightly superior to the solution provided by
the currently used Panel Method. It was also found that the new technique also manages
to obtain better result employing a lower number of nodes during solution, reducing the
computational time. However, the adoption of potential theory means that the stall
conditions of airfoils could still not be predicted at all. |
| format |
Thesis |
| qualification_level |
Master's degree |
| author |
Ahmad Yazid, Aznijar |
| author_facet |
Ahmad Yazid, Aznijar |
| author_sort |
Ahmad Yazid, Aznijar |
| title |
Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
|
| title_short |
Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
|
| title_full |
Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
|
| title_fullStr |
Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
|
| title_full_unstemmed |
Application of Boundary Element Method to Inviscid Flow Around Thin Airfoils
|
| title_sort |
application of boundary element method to inviscid flow around thin airfoils |
| granting_institution |
Universiti Putra Malaysia |
| granting_department |
Faculty of Engineering |
| publishDate |
2004 |
| url |
http://psasir.upm.edu.my/id/eprint/263/1/549489_T_FK_2004_65.pdf |
| _version_ |
1747810186952704000 |