Challenges and opportunities for low noise electric aircraft

E Greenwood, KS Brentner, RF Rau… - International Journal …, 2022 - journals.sagepub.com
A new class of electric aircraft is being developed to transport people and goods as a part of
the urban and regional transportation infrastructure. To gain public acceptance of these …

Computational investigation of microscale coaxial-rotor aerodynamics in hover

VK Lakshminarayan, JD Baeder - Journal of aircraft, 2010 - arc.aiaa.org
MICRO air vehicles (MAVs), as defined in the research program of Defense Advanced
Research Projects Agency (DARPA), are cheap flying vehicles with no dimension exceeding …

Application of vortex methods to coaxial rotor wake and load calculations in hover

P Singh, PP Friedmann - Journal of Aircraft, 2018 - arc.aiaa.org
The coaxial rotor has distinct advantages in hover performance and forward flight compared
to a conventional isolated rotor. The viscous vortex particle approach based on the …

[HTML][HTML] A high-resolution numerical investigation of unsteady wake vortices for coaxial rotors in hover

HAN Shaoqiang, S Wen**, HAN Zhonghua… - Chinese Journal of …, 2024 - Elsevier
High-resolution numerical simulations for wake vortical flows have long been a challenge in
rotor aerodynamics. A novel spectrum-optimized sixth-order Weighted Essentially Non …

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 …

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 …

Performance of a Mach-scale coaxial counter-rotating rotor in hover

CG Cameron, A Karpatne, J Sirohi - Journal of Aircraft, 2016 - arc.aiaa.org
A Mach-scale rotor system, 2.03 m in diameter, was built and hover tested in three
configurations: two-bladed single rotor, four-bladed single rotor, and two-bladed coaxial …

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 …

[HTML][HTML] Aerodynamic analysis of rotor-to-rotor interactions in different octocopter configurations

A Aqib, SHI Yongjie, Y Liu, XU Guohua - Chinese Journal of Aeronautics, 2025 - Elsevier
Rotor-to-rotor interaction among neighboring rotors of a multirotor has great significance for
aerodynamically efficient multirotor design. Current research is conducted to analyze …

Aeromechanics of rigid coaxial rotor models for wind-tunnel testing

JH Schmaus, I Chopra - Journal of Aircraft, 2017 - arc.aiaa.org
A comprehensive analysis for evaluating performance and vibratory loads of a coaxial
helicopter rotor is developed and validated against existing experimental data. The model is …