Predicting aerodynamic rotor-fuselage interactions by using unstructured meshes

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 44, Issue 146, 2002, Pages 208-216

  Lee, Jong Kook ^a   Kwon, Oh Joon ^a  

^a Agency for Defence Development   (South Korea)

Author keywords

Actuator Disk Modeling; Helicopter Aerodynamics; Rotor Fuselage Interaction; Unstructured Meshes

Indexed keywords

COMPUTER SIMULATION; FUSELAGES; HELICOPTER ROTORS; NAVIER STOKES EQUATIONS;

UNSTRUCTURED MESHES;

AERODYNAMICS;

EID: 0036476565     PISSN: 05493811     EISSN: None     Source Type: Journal    
DOI: 10.2322/tjsass.44.208     Document Type: Article

References (19)

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3. An unsteady helicopter rotor-fuselage aerodynamic interaction analysis
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5. Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow
6. Three-dimensional analysis of a rotor in forward flight
7. Navier-Stokes calculations of rotor-airframe interaction in forward flight
8. Numerical simulation of the fuselage-rotor interaction phenomenon
9. Helicopter fuselage aerodynamics under a rotor by Navier-Stokes simulation
10. Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-Meter single rotor
11. Inflow measurement made with a laser velocimeter on a helicopter model in forward flight, volume 1, rectangular planform blades at an advance ratio of 0.15
12. Inflow measurement made with a laser velocimeter on a helicopter model in forward flight, volume 2, rectangular planform blades at an advance ratio of 0.23
13. Characteristic-based schemes for the Euler equations
14. Upwind scheme for solving the Euler equations on unstructured tetrahedral meshes
15. Solution of the 2D Navier-Stokes equations on unstructured adaptive grids
16. Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment