Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed
Also available in printed version
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Bachelor thesis |
| Language: | English |
| Published: |
Universiti Teknologi Malaysia
2025
|
| Subjects: | |
| Online Access: | https://utmik.utm.my/handle/123456789/55390 |
| Abstract | Abstract here |
| _version_ | 1854975083882217472 |
|---|---|
| author | Azrizal Ab. Halim |
| author2 | Md. Nizam Dahalan, supervisor |
| author_facet | Md. Nizam Dahalan, supervisor Azrizal Ab. Halim |
| author_sort | Azrizal Ab. Halim |
| description | Also available in printed version |
| format | Bachelor thesis |
| id | utm-123456789-55390 |
| institution | Universiti Teknologi Malaysia |
| language | English |
| publishDate | 2025 |
| publisher | Universiti Teknologi Malaysia |
| record_format | dspace |
| record_pdf | Abstract |
| spelling | utm-123456789-553902025-08-21T04:01:39Z Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed Azrizal Ab. Halim Md. Nizam Dahalan, supervisor Mechanical engineering Also available in printed version Preliminary design of a supersonic aircraft is an important stage before it could proceed to the detail design. Among so many fields of preliminary design, the interest of this project is converged on the estimation of aerodynamic characteristics of combinations of wing and body configurations. The main target of this project is to find out the estimated lift and drag coefficients for several configuration of wing-body combination of aircraft in supersonic flight regimes. This is also an attempt to develop a software in which the iterating calculations would be programmed into a wizard as to carry out computations with several basic inputs. The result would be displayed in form of the corresponding CL and CD at certain Mach number and angle of attack. Details curve at lift and drag coefficients to the function of angle of attack would also be displayed upon command. The output result of the computer program was compared with wind tunnel test of real aircraft configuration to validate the computer program snhas UTM 66 p. Project Paper (Sarjana Muda Kejuruteraan (Mekanikal - Aeronautik)) - Universiti Teknologi Malaysia, 2015 2025-03-17T03:54:06Z 2025-03-17T03:54:06Z 2015 Bachelor thesis https://utmik.utm.my/handle/123456789/55390 valet-20170131-12268 vital:94555 ENG Closed Access UTM Complete Unpublished application/pdf Universiti Teknologi Malaysia |
| spellingShingle | Mechanical engineering Azrizal Ab. Halim Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| thesis_level | Other |
| title | Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| title_full | Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| title_fullStr | Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| title_full_unstemmed | Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| title_short | Development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| title_sort | development of computer program for aerodynamic characteristics estimation of aircraft at supersonic speed |
| topic | Mechanical engineering |
| url | https://utmik.utm.my/handle/123456789/55390 |
| work_keys_str_mv | AT azrizalabhalim developmentofcomputerprogramforaerodynamiccharacteristicsestimationofaircraftatsupersonicspeed |