[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Prasad et al., 2012 - Google Patents

Finite state inflow models for a coaxial rotor in hover

Prasad et al., 2012

View PDF
Document ID
10821641606857342675
Author
Prasad J
Nowak M
Xin H
Publication year

External Links

Snippet

Formation of a robust, accurate, and computationally efficient induced inflow model is needed to support real time coaxial rotorcraft simulations. Two generalized coaxial rotor models are developed to handle hovering flight condition. One inflow model is obtained by …
Continue reading at dspace-erf.nlr.nl (PDF) (other versions)

Similar Documents

Publication Publication Date Title
Hwang et al. Numerical study of aerodynamic performance of a multirotor unmanned-aerial-vehicle configuration
Theys et al. Wind tunnel testing of a VTOL MAV propeller in tilted operating mode
Khan et al. A propeller model for general forward flight conditions
Qi et al. A study of coaxial rotor aerodynamic interaction mechanism in hover with high-efficient trim model
Lee et al. Review of vortex methods for rotor aerodynamics and wake dynamics
Li et al. CFD calculations on the unsteady aerodynamic characteristics of a tilt-rotor in a conversion mode
Wei et al. Frequency-domain system identification and simulation of a quadrotor controller
Jiang et al. Aerodynamics optimization of a ducted coaxial rotor in forward flight using orthogonal test design
Prasad et al. Finite state inflow models for a coaxial rotor in hover
Koning et al. Using RotCFD to Predict Isolated XV-15 Rotor Performance
Cariglino et al. External aerodynamics simulations in a rotating frame of reference
Lim Consideration of structural constraints in passive rotor blade design for improved performance
Hayami et al. Numerical investigation of aerodynamic interference on coaxial rotor
van der Wall A comprehensive rotary-wing data base for code validation: the HART II international workshop
Yücekayalı Noise minimal & green trajectory and flight profile optimization for helicopters
Lim Consideration of structural constraints in passive rotor blade design for improved performance
Halder et al. Nonlinear aeroelastic coupled trim analysis of a twin cyclocopter in forward flight
Pérez et al. Free-Vortex Wake and CFD Simulation of a Small Rotor for a Quadcopter at Hover
Yeo et al. Experimental characterization of lift on a rigid flapping wing
Geldenhuys Aerodynamic development of a contra-rotating shrouded rotor system for a UAV
Aleksandrov Light-weight multicopter structural design for energy saving
Perez et al. Computational study of a small rotor at hover using CFD and UVLM
Ji et al. Distributed turbulence model with rigorous spatial cross-correlation for simulation of helicopter flight in atmospheric turbulence
Zhao et al. A finite state dynamic wake model enhanced with vortex particle method–derived modeling parameters for coaxial rotor simulation and analysis
Taamallah Flight dynamics modeling for a small-scale flybarless helicopter uav