Aerodynamic design of a medium size blended-wing-body airplane

Tjoetjoek Eko Pambagjo, Kazuhiro Nakahashi, Shigeru Obayashi, Kisa Matsushima

研究成果: Paper査読

4 被引用数 (Scopus)

抄録

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.

本文言語English
出版ステータスPublished - 2001 12 1
イベント39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States
継続期間: 2001 1 82001 1 11

Other

Other39th Aerospace Sciences Meeting and Exhibit 2001
国/地域United States
CityReno, NV
Period01/1/801/1/11

ASJC Scopus subject areas

  • 宇宙惑星科学
  • 航空宇宙工学

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