Vorticity Confinement Technique and Blade Element Method for Accurate Propeller Modelling
Author:
Affiliation:
1. CSIR-National Aerospace Laboratories, Bangalore-560017, India
2. Academy of Scientific and Innovative Research (AcSIR), Ghaziabad-201002, India
Funder
Council of Scientific and Industrial Research
CSIR-National Aerospace Laboratories
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics
Link
https://www.tandfonline.com/doi/pdf/10.1080/10618562.2022.2164276
Reference25 articles.
1. Time Spectral Method for Rotorcraft Flow
2. Frontiers of Computational Fluid Dynamics 2006
3. Analytical solutions for the actuator disk with variable radial distribution of load
4. An automatic anti-diffusion method for vortical flows based on Vorticity Confinement
5. Rotorcraft simulations: a challenge for CFD
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