An experimental investigation of the effects of dynamic motions on a delta wing
The final year project involves the investigation on the vortex breakdown phenomenon associated with dynamic pitching and dynamic rolling delta wing. Experimental investigation was performed on a 70o sweep delta wing with aspect ratio 1.46 at a Reynolds number of 15750in a water tunnel of Nanyang Te...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2012
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/50468 |
| _version_ | 1826124555196825600 |
|---|---|
| author | Yeoh, Chee Wai. |
| author2 | School of Mechanical and Aerospace Engineering |
| author_facet | School of Mechanical and Aerospace Engineering Yeoh, Chee Wai. |
| author_sort | Yeoh, Chee Wai. |
| collection | NTU |
| description | The final year project involves the investigation on the vortex breakdown phenomenon associated with dynamic pitching and dynamic rolling delta wing. Experimental investigation was performed on a 70o sweep delta wing with aspect ratio 1.46 at a Reynolds number of 15750in a water tunnel of Nanyang Technological University. The vortex breakdown location of delta wing under steady state and dynamic motion was visualized using dye injection. |
| first_indexed | 2024-10-01T06:22:15Z |
| format | Final Year Project (FYP) |
| id | ntu-10356/50468 |
| institution | Nanyang Technological University |
| language | English |
| last_indexed | 2024-10-01T06:22:15Z |
| publishDate | 2012 |
| record_format | dspace |
| spelling | ntu-10356/504682023-03-04T19:22:59Z An experimental investigation of the effects of dynamic motions on a delta wing Yeoh, Chee Wai. School of Mechanical and Aerospace Engineering New Tze How, Daniel DRNTU::Engineering::Aeronautical engineering::Aerodynamics The final year project involves the investigation on the vortex breakdown phenomenon associated with dynamic pitching and dynamic rolling delta wing. Experimental investigation was performed on a 70o sweep delta wing with aspect ratio 1.46 at a Reynolds number of 15750in a water tunnel of Nanyang Technological University. The vortex breakdown location of delta wing under steady state and dynamic motion was visualized using dye injection. Bachelor of Engineering (Aerospace Engineering) 2012-06-06T01:30:00Z 2012-06-06T01:30:00Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50468 en Nanyang Technological University 71 p. application/pdf |
| spellingShingle | DRNTU::Engineering::Aeronautical engineering::Aerodynamics Yeoh, Chee Wai. An experimental investigation of the effects of dynamic motions on a delta wing |
| title | An experimental investigation of the effects of dynamic motions on a delta wing |
| title_full | An experimental investigation of the effects of dynamic motions on a delta wing |
| title_fullStr | An experimental investigation of the effects of dynamic motions on a delta wing |
| title_full_unstemmed | An experimental investigation of the effects of dynamic motions on a delta wing |
| title_short | An experimental investigation of the effects of dynamic motions on a delta wing |
| title_sort | experimental investigation of the effects of dynamic motions on a delta wing |
| topic | DRNTU::Engineering::Aeronautical engineering::Aerodynamics |
| url | http://hdl.handle.net/10356/50468 |
| work_keys_str_mv | AT yeohcheewai anexperimentalinvestigationoftheeffectsofdynamicmotionsonadeltawing AT yeohcheewai experimentalinvestigationoftheeffectsofdynamicmotionsonadeltawing |