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

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

Research output: Contribution to conferencePaperpeer-review

3 Citations (Scopus)

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 languageEnglish
Publication statusPublished - 2001 Dec 1
Event39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States
Duration: 2001 Jan 82001 Jan 11

Other

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

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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