Airfoil Optimization And 3D Rotor Aerodynamics Exploration For Mars Helicopter Using Direct Numerical Simulation

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dc.contributor.authorPark, S.
dc.contributor.authorWilke, G.
dc.contributor.authorHong, Y.
dc.contributor.authorYee, K.
dc.date.accessioned2026-08-14T09:35:00Z
dc.date.issued2025
dc.description.abstractA one-paragraph abstract of approximately 150 words is required. It should be a summary, not an introduction, and be complete in itself. It should not contain any numerical references to figures or references contained in the paper. The abstract should indicate the subject covered in the paper and should state the objectives of the investigation. Newly observed facts and conclusions must be stated in summary form. Readers should not have to read the paper to understand the abstract.
dc.identifier.citation51st European Rotorcraft Forum (ERF 2025), September 9-12, 2025, Venice, Italy : proceeedings. ISBN 9798331335472.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4805
dc.language.isoen
dc.titleAirfoil Optimization And 3D Rotor Aerodynamics Exploration For Mars Helicopter Using Direct Numerical Simulation

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