Airfoil optimization methodology and CFD validation for Mars atmospheric conditions

Author:

Strelets DmitryORCID,Parkhaev Egor,Fevralskikh Andrey,Gueraiche Djahid,Das Debopam

Funder

Russian Science Fund

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Reference21 articles.

1. Masayuki A, Kei N, Shingo I, Daiju N, Hiroki N, Keisuke A (2010) Low reynolds number airfoil testing in a mars wind tunnel. In: 40th Fluid dynamics conference and exhibit, p 4627

2. Yang H, Agarwal RK (2019) CFD simulations of a triangular airfoil for Martian atmosphere in low-reynolds number compressible flow. In: AIAA Aviation 2019 Forum, p 2923

3. Koning WJ, Romander EA, Johnson W (2020) Optimization of low Reynolds number airfoils for martian rotor applications using an evolutionary algorithm. In: AIAA Scitech 2020 Forum, p 0084

4. Lorenz RD, Turtle EP, Barnes JW, Trainer MG, Adams DS, Hibbard KE, Bedini PD (2018) Dragonfly: A rotorcraft lander concept for scientific exploration at Titan. Johns Hopkins APL Tech Dig 34(3):14

5. Seeman GR (1978) A Concept Study of a Remotely Piloted Vehicle for Mars Exploration. NASA CR, 157942

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