Actuator Surface Model with Computational-Fluid-Dynamics-Convected Wake Model for Rotorcraft Applications
Author:
Affiliation:
1. University of Sydney, Sydney, New South Wales 2006, Australia
2. Defence Science and Technology Organisation, Fishermans Bend, Victoria 3207, Australia
Funder
Defence Science and Technology Group
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference49 articles.
1. Modern helicopter rotor aerodynamics
2. Three Dimensional Analysis of a Rotor in Forward Flight
3. Numerical Modeling of Wind Turbine Wakes
4. The Actuator Surface Model: A New Navier–Stokes Based Model for Rotor Computations
5. Coupled flight dynamics and CFD – demonstration for helicopters in shipborne environment
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1. Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface;Journal of Aircraft;2024-05-12
2. Comparative Analysis of Direct Method and Fast Multipole Method for Multirotor Wake Dynamics;International Journal of Aeronautical and Space Sciences;2024-01-10
3. Simulation of Rotorcraft Fuselage with Rotor Effects Using An Immersed Boundary Method;Journal of the American Helicopter Society;2023-04-01
4. Accuracy of the new actuator surface-CFD approach for predicting the performance of oscillating turbines;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2022-12-10
5. Investigation of a Virtual Blade Method for Aerodynamic and Acoustic Prediction of Helicopter Rotors;International Journal of Aeronautical and Space Sciences;2022-12-09
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