Direct Numerical Simulation of Flow over a Triangular Airfoil Under Martian Conditions
Author:
Affiliation:
1. Imperial College London, London, England SW7 2AZ, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061454
Reference13 articles.
1. Improved Mars Helicopter Aerodynamic Rotor Model for Comprehensive Analyses
2. Computational and Experimental Analysis of a High-Performance Airfoil Under Low-Reynolds-Number Flow Condition
3. Flow Visualization Study of the Aerodynamics of Modeled Dragonfly Wings
4. Experimental Study on Aerodynamic Characteristics of Unsteady Wings at Low Reynolds Number
5. An Experimental Study of Triangular Airfoils for Mars Airplane
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