[go: up one dir, main page]

Lefevre et al., 2022 - Google Patents

Experimental evaluation of the aerodynamic rotor/propeller interactions on high speed helicopters, efforts and velocity fields measurements

Lefevre et al., 2022

View PDF
Document ID
156307705128282723
Author
Lefevre L
Nowinski V
Delva J
Dazin A
Publication year
Publication venue
VFS 78th Forum

External Links

Snippet

This paper focuses on the experimental evaluation of the rotor/propeller interactions for hybrid compound configurations. Experiments are conducted in the ONERA L2 large size- low speed wind tunnel with a 1/7.7 Dauphin 365N model and a four-bladed small-scale …
Continue reading at hal.science (PDF) (other versions)

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter

Similar Documents

Publication Publication Date Title
Roskam Airplane design
Serrano et al. Effect of disk angle-of-attack on aerodynamic performance of small propellers
Jardin et al. Aerodynamic performance of a hovering microrotor in confined environment
McCroskey Measurements of boundary layer transition, separation and streamline direction on rotating blades
Kaya et al. Aerodynamic modeling and parameter estimation of a quadrotor helicopter
US5595357A (en) Aircraft stall warning system
Moffitt et al. Validation of vortex propeller theory for UAV design with uncertainty analysis
Lefevre et al. Experimental evaluation of the aerodynamic rotor/propeller interactions on high speed helicopters, efforts and velocity fields measurements
Eraslan et al. A literature review on determination of quadrotor unmanned aerial vehicles propeller thrust and power coefficients
Czyz et al. Aerodynamic characteristics of the X-tail stabilizer in a hybrid unmanned aircraft
Lefevre et al. Experimental evaluation of the aerodynamic rotor/propeller interactions in hybrid compound helicopters
Awad et al. Aero-propulsive interaction model for conceptual distributed propulsion aircraft design
Riccobene et al. Wind tunnel test of full-scale wing-propeller system of a eVTOL aircraft
Ham Some Conclusions from an Investigation of Blade‐Vortex Interaction
Chen et al. Tip vortex trajectory and its application in small-rotor/wing interaction
Chen et al. Prediction of dual-rotor-wing interaction in hover using actuator disk theory
Yokota et al. Observer-based angle of attack estimation for tilt-wing eVTOL aircraft
Lefevre et al. Experimental velocity fields evaluation of the rotor/propeller interactions for high-speed helicopters with different propeller positions
LEFEVRE et al. Experimental Velocity Fields Evaluation under the Rotor/Propeller Interactions for High Speed Helicopters for Different Propeller Positions
Ye et al. Rotor performance analysis and modeling of multirotor using wind-tunnel test
Lauriane et al. Characterization of the propeller for the experimental evaluation of the aerodynamic rotor/propeller interactions in hybrid compound helicopters
Leng et al. Slipstream deformation of a propeller-wing combination applied for convertible uavs in hover condition
Cook et al. Comparison of Wind-Tunnel and Flight-Test Aerodynamic Data in the Transition-Flight Speed Range for Five V/STOL Aircraft
Leng et al. Comparisons of different propeller wake models for a propeller-wing combination
Bryant et al. Developing a Small-Scale Propeller Thrust Model Using Experimentation and CFD