Design of Supercritical Low-Reynolds-Number Airfoils for Fixed-Wing Flight on Mars
Author:
Affiliation:
1. Engineering Dept., Aeronautical and Mechanical Engineering Div., Univ. of Salford, Salford M5 4WT, UK (corresponding author).
2. Engineering Dept., Aeronautical and Mechanical Engineering Div., Univ. of Salford, Salford M5 4WT, UK. ORCID:
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001166
Reference32 articles.
1. Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows
2. Biber K. and C. P. Tilmann. 2003. “Supercritical airfoil design for future HALE concepts.” In Proc. 41st Aerospace Sciences Meeting and Exhibit Paper 2003-1095. Reno NV: American Institute for Aeronautics and Astronautics.
3. Design of the ARES Mars Airplane and Mission Architecture
4. Continuous Adjoint Approach for the Spalart-Allmaras Model in Aerodynamic Optimization
5. A correlation-based algebraic transition model
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