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

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

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

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

Creative Flow Research Division

Research output: Contribution to conference › Paper › peer-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 language	English
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
Country	United States
City	Reno, NV
Period	01/1/8 → 01/1/11

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

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Cite this

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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.",

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AU - Pambagjo, Tjoetjoek Eko

AU - Nakahashi, Kazuhiro

AU - Obayashi, Shigeru

AU - Matsushima, Kisa

PY - 2001/12/1

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N2 - 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.

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