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Case Study on Aerodynamics Stability of Bixel Wing-In-Ground Effect Craft
| Content Provider | Scilit |
|---|---|
| Author | Pua’At, Afifi.A Matdaud, Zulkifli Zhahir, Amzari Ahmad, Mohamed Tarmizi Hassan, Aziz |
| Copyright Year | 2019 |
| Description | Journal: Iop Conference Series: Materials Science and Engineering Wing-in-ground effect (WIG) crafts fly efficiently by exploiting the ground effect i.e. generating a notable rise in the lift-over-drag ratio when a three-dimensional wing approaches a large flat plane either water or ground surface. A successful WIG craft will create another mode of transportation categorise in between commercial airplanes and marine vessels. Hence, this paper presents a case study of Bixel Wing-In-Ground-Effect aerodynamic (Bixel WIG). The initial task is to simulate Bixel WIG aerodynamic using XFLR5 software. The craft configuration is a double wing flat aerofoil wave rider design with aspect ratio variation from 0.25 to 0.5 as in USA PATENT #5105898 C.BIXEL. Based on the result of the simulation, the design of the six seater double wing Bixel WIG is proposed. The design is benchmarked against Lippisch RHB X-114 and UH-18 SPW. |
| Related Links | https://iopscience.iop.org/article/10.1088/1757-899X/642/1/012001/pdf |
| ISSN | 17578981 |
| e-ISSN | 1757899X |
| DOI | 10.1088/1757-899x/642/1/012001 |
| Journal | Iop Conference Series: Materials Science and Engineering |
| Issue Number | 1 |
| Volume Number | 642 |
| Language | English |
| Publisher | IOP Publishing |
| Publisher Date | 2019-10-01 |
| Access Restriction | Open |
| Subject Keyword | Journal: Iop Conference Series: Materials Science and Engineering Transportation Science and Technology Ground Effect Bixel Wing Double Wing |
| Content Type | Text |
| Resource Type | Article |
