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 …
range of applications. Design parameters are identified that effect the fundamental …
Numerical investigation of aerodynamic interactions for the coaxial rotor system in low-speed forward flight
X Yuan, W Bian, Q Zhao, G Zhao - Aerospace Science and Technology, 2024 - Elsevier
This study is conducted to investigate the aerodynamic characteristics of a coaxial rotor in
low-speed forward flight using a high-fidelity computational fluid dynamics (CFD) solver …
low-speed forward flight using a high-fidelity computational fluid dynamics (CFD) solver …
Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method
P Singh - 2020 - deepblue.lib.umich.edu
Coaxial rotor helicopters are a candidate for the next generation of rotorcraft due to their
ability to achieve high speeds without compromising hover performance. Coaxial rotors are …
ability to achieve high speeds without compromising hover performance. Coaxial rotors are …
Time-varying loads of co-axial rotor blade crossings
NL Schatzman, N Komerath… - SAE International Journal …, 2017 - ntrs.nasa.gov
The blade crossing event of a coaxial counter-rotating rotor is a potential source of noise
and impulsive blade loads. Blade crossings occur many times during each rotor revolution …
and impulsive blade loads. Blade crossings occur many times during each rotor revolution …
Modeling Shed Vorticity from Coaxial Blade Interactions
NL Schatzman, EA Romander… - 2018 Fluid Dynamics …, 2018 - arc.aiaa.org
Vr/R= velocity at r/R spanwise location (m/s) Vtip= rotor blade rotational speed at tip (m/s)
V∞= forward flight velocity (m/s) α= airfoil angle-of-attack (deg), positive pitch up Γ= vortex …
V∞= forward flight velocity (m/s) α= airfoil angle-of-attack (deg), positive pitch up Γ= vortex …