Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane

Koji Shimoyama; Akira Oyama; Kozo Füjii

doi:10.2514/6.iac-06-a3.p.3.07

Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane

Koji Shimoyama, Akira Oyama, Kozo Füjii

Creative Flow Research Division

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

3 Citations (Scopus)

Abstract

Robust aerodynamic airfoil design optimizations of Mars exploratory airplane against wind variations have been carried out by using DFMOSS coupled with the CFD simulation. The present robust optimizations successfully found the airfoil designs with robust aerodynamic performances against wind variations. Obtained airfoil design information about the optimality and the robustness of aerodynamic performances indicated that an airfoil with smaller camber can improve the robustness in lift to drag ratio against the variation of flight Mach number, and an airfoil with larger curvature near the shock wave location can improve the robustness in pitching moment against the variation of flight Mach number.

Original language	English
Title of host publication	AIAA 57th International Astronautical Congress, IAC 2006
Publisher	American Institute of Aeronautics and Astronautics Inc.
Pages	1494-1500
Number of pages	7
ISBN (Print)	9781605600390
DOIs	https://doi.org/10.2514/6.iac-06-a3.p.3.07
Publication status	Published - 2006
Event	AIAA 57th International Astronautical Congress, IAC 2006 - Valencia, Spain Duration: 2006 Oct 2 → 2006 Oct 6

Publication series

Name	AIAA 57th International Astronautical Congress, IAC 2006
Volume	3

Other

Other	AIAA 57th International Astronautical Congress, IAC 2006
Country/Territory	Spain
City	Valencia
Period	06/10/2 → 06/10/6

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

Access to Document

10.2514/6.iac-06-a3.p.3.07

Cite this

Shimoyama, K., Oyama, A., & Füjii, K. (2006). Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane. In AIAA 57th International Astronautical Congress, IAC 2006 (pp. 1494-1500). (AIAA 57th International Astronautical Congress, IAC 2006; Vol. 3). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.iac-06-a3.p.3.07

Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane. / Shimoyama, Koji; Oyama, Akira; Füjii, Kozo.
AIAA 57th International Astronautical Congress, IAC 2006. American Institute of Aeronautics and Astronautics Inc., 2006. p. 1494-1500 (AIAA 57th International Astronautical Congress, IAC 2006; Vol. 3).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Shimoyama, K, Oyama, A & Füjii, K 2006, Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane. in AIAA 57th International Astronautical Congress, IAC 2006. AIAA 57th International Astronautical Congress, IAC 2006, vol. 3, American Institute of Aeronautics and Astronautics Inc., pp. 1494-1500, AIAA 57th International Astronautical Congress, IAC 2006, Valencia, Spain, 06/10/2. https://doi.org/10.2514/6.iac-06-a3.p.3.07

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doi = "10.2514/6.iac-06-a3.p.3.07",

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Robust aerodynamic airfoil design optimization against wind variations for mars exploratory airplane

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