Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER). [PDF]
Abedini A, Bataleblu AA, Roshanian J.
europepmc +1 more source
Vorticity-transport and unstructured RANS investigation of rotor-fuselage interactions [PDF]
The prediction capabilities of unstructured primitive-variable and vorticity-transport-based Navier-Stokes solvers have been compared for rotorcraft-fuselage interaction.
Brown, Richard +3 more
core
Modeling and Simulation of Coaxial Helicopter Rotor Aerodynamics
A framework is developed for the computational fluid dynamics (CFD) analyses of a series of helicopter rotor flowfields in hover and in forward flight. The methodology is based on the unsteady solutions of the three-dimensional, compressible Navier-Stokes equations recast in a rotating frame of reference.
openaire +2 more sources
Dynamic modeling and analysis of the rotor-stator coupling system of a coaxial contra-rotating gearbox. [PDF]
Zhang D, Cui J, Zhu R, Li M.
europepmc +1 more source
Dynamic Electromagnetic Scattering Simulation of Tilt-Rotor Aircraft in Multiple Modes. [PDF]
Fei Z, Yang Y, Jiang X, Zhao Q, Chen X.
europepmc +1 more source
In recent years, multirotor unmanned aerial vehicles (MRUAVs) have seen increased investment and deployment for various novel uses, including intruder surveillance, agro farming, and crack detection in severe environments.
Beena Stanislaus Arputharaj +9 more
doaj +1 more source
A Study of Coaxial Rotor Performance and Flow Field Characteristics [PDF]
As a precursor to studying the acoustics of a coaxial rotor system, the aerodynamics and flow field of a coaxial rotor were simulated to better understand the interaction between the two rotors.
Barbely, Natasha L. +2 more
core +1 more source
Improvement of the Airflow Energy Harvester Based on the New Diamagnetic Levitation Structure. [PDF]
Zhang L +5 more
europepmc +1 more source
COAXIAL ROTOR SYSTEMS – CHARACTERISTICS AND PERFORMANCES
Constantin ROTARU +3 more
openaire +1 more source
Acoustic measurements of a full-scale coaxial hingeless rotor helicopter [PDF]
Acoustic data were obtained during a full-scale test of the XH-59A Advancing Blade Concept Technology Demonstrator in the 40- by 80-Foot Wind Tunnel. The XH-59A is a research helicopter with two coaxial rotors and hingeless blades. Performance, vibration,
Mosher, M., Peterson, R. L.
core +1 more source

