Abstract
This paper presents the aerodynamic design process of a Blended-Wing-Body airplane for 200 passengers. The wing is designed by using Takanashi's inverse design method where the target pressure distributions are specified by using the constrained target pressure specification technique. RAPID methodology is utilized to obtain a smooth wing surface. This study shows that the combination of those three design tools works well to design the Blended-Wing-Body airplane configuration.
Original language | English |
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Publication status | Published - 2001 Dec 1 |
Event | 39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States Duration: 2001 Jan 8 → 2001 Jan 11 |
Other
Other | 39th Aerospace Sciences Meeting and Exhibit 2001 |
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Country | United States |
City | Reno, NV |
Period | 01/1/8 → 01/1/11 |
ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering