Numerical Investigation on Aerodynamics of a Rectangular Blade Rotor under Mars Air Conditions Using Large Eddy Simulation
The study of the aerodynamics of a flight vehicle under Martian air conditions is experimentally difficult due to its characteristics such as low air density and temperature, making the vehicle operate at an ultra-low Reynolds number, which in turn introduces a complex flow field. In this paper, to...
Main Authors: | Jie Huang, Daqing Huang, Tao Chen, Hongda Li |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-04-01
|
Series: | Applied Sciences |
Subjects: | |
Online Access: | https://www.mdpi.com/2076-3417/13/8/5058 |
Similar Items
-
A Hybrid Non-Linear Unsteady Vortex Lattice-Vortex Particle Method for Rotor Blades Aerodynamic Simulations
by: Vincent Proulx-Cabana, et al.
Published: (2022-02-01) -
Machine Learning Assisted Prediction of Airfoil Lift-to-Drag Characteristics for Mars Helicopter
by: Pengyue Zhao, et al.
Published: (2023-07-01) -
Earth – Mars Similarity Criteria for Martian Vehicles
by: Octavian TRIFU, et al.
Published: (2010-09-01) -
Aerodynamic study of helicopter main rotor blade in hovering flight /
by: 454632 Mohd. Fadhli Nadzri
Published: (2003) -
COMPUTATIONAL STUDIES OF HELICOPTER AERODYNAMICS
by: Marcel ILIE, et al.
Published: (2023-06-01)