Hovering Helicopter Rotors Modeling Using the Actuator Line Method-Reference-Cited by-同舟云学术

Hovering Helicopter Rotors Modeling Using the Actuator Line Method

Published:2021-10-25 Issue: Volume: Page:1-14
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Merabet Reda¹,Laurendeau Eric¹

Affiliation:

1. Polytechnique Montreal, Montreal, Quebec H3T 1J4, Canada

Funder

CAE inc.

Natural Sciences and Engineering Research Council of Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036314

Reference41 articles.

1. Time-Accurate Ship Airwake and Unsteady Aerodynamic Loads Modeling for Maritime Helicopter Simulation

2. Integrating CFD and piloted simulation to quantify ship-helicopter operating limits

3. Numerical Study of Helicopter Rotors in a Ship Airwake

4. QuackenbushR.ChuaK.WachspressD. A.BoschitschH. “Computation of Rotor Aerodynamic Loads in Forward Flight Using a Full-Span Free Wake Analysis,” NASA CR 77611, Oct. 1990.

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