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Volumn 58, Issue 5, 2008, Pages 527-549

Sliding mesh algorithm for CFD analysis of helicopter rotor-fuselage aerodynamics

Author keywords

Mesh deformation; Rotor fuselage interaction; Rotorcraft CFD; Sliding planes

Indexed keywords

AERODYNAMICS; AIR; COMPUTATIONAL FLUID DYNAMICS; DEFORMATION; DYNAMICS; FLOW INTERACTIONS; FLUID DYNAMICS; FUSELAGES; GAS DYNAMICS; HELICOPTERS;

EID: 57849094969     PISSN: 02712091     EISSN: 10970363     Source Type: Journal    
DOI: 10.1002/fld.1757     Document Type: Article
Times cited : (243)

References (25)
  • 1
    • 0037521722 scopus 로고
    • Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-meter diameter single rotor
    • Freeman CE, Mineck RE. Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-meter diameter single rotor. NASA TM-80051, 1979.
    • (1979) NASA , vol.TM-80051
    • Freeman, C.E.1    Mineck, R.E.2
  • 2
    • 0003223160 scopus 로고
    • Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
    • June
    • Chaffin MS, Berry JD. Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment. NASA TM-4566, June 1994.
    • (1994) NASA , vol.TM-4566
    • Chaffin, M.S.1    Berry, J.D.2
  • 3
    • 0001575894 scopus 로고
    • A conservative treatment of zonal boundaries for Euler equation calculations
    • Rai M. A conservative treatment of zonal boundaries for Euler equation calculations. Journal of Computational Physics 1986; 62:472-503.
    • (1986) Journal of Computational Physics , vol.62 , pp. 472-503
    • Rai, M.1
  • 4
    • 38249039018 scopus 로고
    • A relaxation approach to patched-grid calculations with the Euler equations
    • Rai M. A relaxation approach to patched-grid calculations with the Euler equations. Journal of Computational Physics 1986; 66:99-131.
    • (1986) Journal of Computational Physics , vol.66 , pp. 99-131
    • Rai, M.1
  • 5
    • 0041649591 scopus 로고    scopus 로고
    • A fully distributed unstructured Navier-Stokes solver for large-scale aeroelasticity computations
    • Barakos G, Vahdati M, Sayma AI, Breard C, Imregun M. A fully distributed unstructured Navier-Stokes solver for large-scale aeroelasticity computations. The Aeronautical Journal 2001; 105:419-426.
    • (2001) The Aeronautical Journal , vol.105 , pp. 419-426
    • Barakos, G.1    Vahdati, M.2    Sayma, A.I.3    Breard, C.4    Imregun, M.5
  • 6
    • 48749145864 scopus 로고
    • Upwind schemes and boundary conditions with applications to Euler equations in general geometries
    • Osher S, Chakravarthy S. Upwind schemes and boundary conditions with applications to Euler equations in general geometries. Journal of Computational Physics 1983; 50:447-481.
    • (1983) Journal of Computational Physics , vol.50 , pp. 447-481
    • Osher, S.1    Chakravarthy, S.2
  • 7
    • 49049151571 scopus 로고
    • Flux vector splitting of the inviscid gasdynamics equations with application to finite-difference methods
    • Steger JL, Warming RF. Flux vector splitting of the inviscid gasdynamics equations with application to finite-difference methods. Journal of Computational Physics 1981; 40:263-293.
    • (1981) Journal of Computational Physics , vol.40 , pp. 263-293
    • Steger, J.L.1    Warming, R.F.2
  • 9
    • 4143065683 scopus 로고    scopus 로고
    • Calculation of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling
    • Moscow, Russia, September
    • Pahlke K, Van der Wall B. Calculation of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling. Twenty-seventh European Rotorcraft Forum, Moscow, Russia, September 2001.
    • (2001) Twenty-seventh European Rotorcraft Forum
    • Pahlke, K.1    Van der Wall, B.2
  • 10
    • 4143086039 scopus 로고    scopus 로고
    • Navier-Stokes computations of a complete helicopter configuration accounting for main and tail rotor effects
    • Friedrichshafen, Germany, September
    • Renaud T, Benoit C, Boniface J-C, Gardarein P. Navier-Stokes computations of a complete helicopter configuration accounting for main and tail rotor effects. Twenty-ninth European Rotorcraft Forum, Friedrichshafen, Germany, September 2003.
    • (2003) Twenty-ninth European Rotorcraft Forum
    • Renaud, T.1    Benoit, C.2    Boniface, J.-C.3    Gardarein, P.4
  • 11
    • 3042792928 scopus 로고    scopus 로고
    • Aeroelastic analysis of helicopter rotor blades on deformable chimera grids
    • Pomin H, Wagner S. Aeroelastic analysis of helicopter rotor blades on deformable chimera grids. Journal of Aircraft 2004; 41(3):577-584.
    • (2004) Journal of Aircraft , vol.41 , Issue.3 , pp. 577-584
    • Pomin, H.1    Wagner, S.2
  • 13
    • 2942735812 scopus 로고    scopus 로고
    • Simulation of unsteady rotor-fuselage aerodynamic interaction using unstructured adaptive meshes
    • Phoenix, AZ, 6-8 May
    • Park Y, Nam HJ, Kwon OJ. Simulation of unsteady rotor-fuselage aerodynamic interaction using unstructured adaptive meshes. Fifty-ninth Annual Forum of the American Helicopter Society, Phoenix, AZ, 6-8 May 2003.
    • (2003) Fifty-ninth Annual Forum of the American Helicopter Society
    • Park, Y.1    Nam, H.J.2    Kwon, O.J.3
  • 14
    • 8644285054 scopus 로고    scopus 로고
    • Simulation of unsteady rotor flow field using unstructured adaptive sliding meshes
    • Park Y, Kwon OJ. Simulation of unsteady rotor flow field using unstructured adaptive sliding meshes. Journal of the American Helicopter Society 2004; 49(4):391-400.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.4 , pp. 391-400
    • Park, Y.1    Kwon, O.J.2
  • 15
    • 33744530556 scopus 로고    scopus 로고
    • Simulation of unsteady rotor-fuselage aerodynamic interaction using unstructured adaptive meshes
    • Nam HJ, Park Y, Kwon OJ. Simulation of unsteady rotor-fuselage aerodynamic interaction using unstructured adaptive meshes. Journal of the American Helicopter Society 2006; 51(2):141-148.
    • (2006) Journal of the American Helicopter Society , vol.51 , Issue.2 , pp. 141-148
    • Nam, H.J.1    Park, Y.2    Kwon, O.J.3
  • 18
    • 34250847710 scopus 로고    scopus 로고
    • CFD analysis of rotor-fuselage interactional aerodynamics
    • Reno, Nevada, U.S.A, 8-11 January, AIAA Paper 2007-1278
    • Steijl R, Barakos G. CFD analysis of rotor-fuselage interactional aerodynamics. Forty-fifth AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., 8-11 January 2007; AIAA Paper 2007-1278.
    • (2007) Forty-fifth AIAA Aerospace Sciences Meeting and Exhibit
    • Steijl, R.1    Barakos, G.2
  • 19
    • 0343228755 scopus 로고    scopus 로고
    • Elements of computational fluid dynamics on block structured grids using implicit solvers
    • Badcock K, Richards B, Woodgate M. Elements of computational fluid dynamics on block structured grids using implicit solvers. Progress in Aerospace Sciences 2000; 36(5-6):351-392.
    • (2000) Progress in Aerospace Sciences , vol.36 , Issue.5-6 , pp. 351-392
    • Badcock, K.1    Richards, B.2    Woodgate, M.3
  • 20
    • 0004261656 scopus 로고
    • Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
    • AIAA Paper, 91-1596
    • Jameson A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings. AIAA Paper, 91-1596, 1991.
    • (1991)
    • Jameson, A.1
  • 21
    • 12744279431 scopus 로고    scopus 로고
    • Aerofoil-vortex interaction using the compressible vorticity confinement method
    • Morvant R, Badcock K, Barakos G, Richards BE. Aerofoil-vortex interaction using the compressible vorticity confinement method. AIAA Journal 2004; 43(1):63-75.
    • (2004) AIAA Journal , vol.43 , Issue.1 , pp. 63-75
    • Morvant, R.1    Badcock, K.2    Barakos, G.3    Richards, B.E.4
  • 24
    • 57849086348 scopus 로고    scopus 로고
    • Mineck RE, Althoff Gorton S. Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor. NASA TM 210286, 2000.
    • Mineck RE, Althoff Gorton S. Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor. NASA TM 210286, 2000.
  • 25
    • 57849129231 scopus 로고    scopus 로고
    • Elliot JW, Althoff SL, Sailey RH. Inflow measurements made with a laser velocimeter on a helicopter model in forward flight, 1, Rectangular planform blades at an advance ratio of 0.15. NASA TM 100541, 1988.
    • Elliot JW, Althoff SL, Sailey RH. Inflow measurements made with a laser velocimeter on a helicopter model in forward flight, Volume 1, Rectangular planform blades at an advance ratio of 0.15. NASA TM 100541, 1988.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.