A study of coaxial rotor aerodynamic interaction mechanism in hover with high-efficient trim model

H Qi, G Xu, C Lu, Y Shi - Aerospace Science and Technology, 2019 - Elsevier
A numerical method based on Reynolds Averaged Navier–Stokes (RANS) equations and
moving overset mesh technique is developed to simulate the aerodynamics of Harrington …

High-fidelity aeromechanical analysis of coaxial mars helicopter

D Escobar, I Chopra, A Datta - Journal of Aircraft, 2021 - arc.aiaa.org
A high-fidelity coupled computational fluid dynamics and comprehensive analysis solver is
developed for helicopter flight on Mars. The objectives are accurate prediction of flight loads …

Efficient computational fluid dynamics approach for coaxial rotor simulations in hover

JK Cornelius, S Schmitz, MP Kinzel - Journal of aircraft, 2021 - arc.aiaa.org
SMALL-SCALE multicopter aircraft are continually seen more in many aspects of society,
and their applications stretch far beyond a commercial product. The increasing demand for …

Investigation of rotor efficiency with varying rotor pitch angle for a coaxial drone

KET Giljarhus, A Porcarelli, J Apeland - Drones, 2022 - mdpi.com
Coaxial rotor systems are appealing for multirotor drones, as they increase thrust without
increasing the vehicle's footprint. However, the thrust of a coaxial rotor system is reduced …

Three-Dimensional Aeromechanical Analysis of Lift Offset Coaxial Rotors: A Helios Test Case

M Patil, A Datta - Journal of Aircraft, 2024 - arc.aiaa.org
Three-dimensional (3-D) solid finite element analysis (FEA) is used to model and study
coaxial helicopter rotors. The 3-D FEA is coupled with a lifting line aerodynamic model with …

Geometry Design of Coaxial Rigid Rotor in High‐Speed Forward Flight

B Wang, X Yuan, Q Zhao, Z Zhu - International Journal of …, 2020 - Wiley Online Library
The aerodynamic performance analysis and blade planform design of a coaxial rigid rotor in
forward flight were carried out utilizing CFD solver CLORNS. Firstly, the forward flow field …

Aerodynamics and aeroacoustic sources of a coaxial rotor

NL Schatzman - 2018 - ntrs.nasa.gov
Vehicles with coaxial, contra-rotating rotor systems (CACR) are being considered for a
range of applications. Design parameters are identified that effect the fundamental …

Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover

P Mortimer, J Sirohi, S Platzer, J Rauleder - Journal of Aircraft, 2023 - arc.aiaa.org
The flowfield of a coaxial counter-rotating rotor in hover was measured using particle image
velocimetry. The goal of the measurements was to investigate the flow features of coaxial …

[图书][B] The effects of coaxial propellers for the propulsion of multirotor systems

JE Holzsager - 2017 - search.proquest.com
Multirotor vehicles offer access to the skies for users across all walks of life and industry due
to their simplicity, availability, and low cost. Although advancements continue, developers …

Coaxial rotor flow phenomena in forward flight

NL Barbely, NM Komerath - 2016 International Powered Lift …, 2016 - ntrs.nasa.gov
Coaxial rotors are nding use in advanced rotorcraft concepts. Combined with lift offset rotor
technology, they offer a solution to the problems of dynamic stall and re-verse ow that often …