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Volumn 2005, Issue , 2005, Pages 1-10

Influence of wind-tunnel walls in helicopter aerodynamics predictions

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL COMPLEXITY; COMPUTER SIMULATION; EMBEDDED SYSTEMS; FUSELAGES; HELICOPTER ROTORS; WIND TUNNELS;

EID: 33746643437     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (22)
  • 5
    • 0035606970 scopus 로고    scopus 로고
    • Numerical simulation of flows around helicopters at DLR and ONERA
    • Sidès J., Pahlke K., Costes M. (2001). Numerical simulation of flows around helicopters at DLR and ONERA, Aerosp. Sci. Technol., 5, 35-53.
    • (2001) Aerosp. Sci. Technol. , vol.5 , pp. 35-53
    • Sidès, J.1    Pahlke, K.2    Costes, M.3
  • 6
  • 10
    • 0042882695 scopus 로고    scopus 로고
    • Unsteady overset simulation of rotor-airframe interaction
    • Hariharan N., Sankar L.N. (2003). Unsteady Overset Simulation of Rotor-Airframe Interaction, J. of Aircraft, 40, 662-674.
    • (2003) J. of Aircraft , vol.40 , pp. 662-674
    • Hariharan, N.1    Sankar, L.N.2
  • 13
    • 84982318200 scopus 로고
    • An efficient means of adaptive refinement within systems of overset grids
    • Meakin R.L. (1995). An Efficient Means of Adaptive Refinement Within Systems of Overset Grids, AIAA Paper 95-1722-CP, 844-857.
    • (1995) AIAA Paper 95-1722-CP , pp. 844-857
    • Meakin, R.L.1
  • 14
    • 0034730338 scopus 로고    scopus 로고
    • Adaptive spatial partitioning and refinement for overset structured grids
    • Meakin R.L. (2000). Adaptive spatial partitioning and refinement for overset structured grids, Comput. Methods Appl. Mech. Eng., 189, 1077-1117.
    • (2000) Comput. Methods Appl. Mech. Eng. , vol.189 , pp. 1077-1117
    • Meakin, R.L.1
  • 15
    • 0038363560 scopus 로고    scopus 로고
    • Three-dimensional inviscid isolated rotor calculations using chimera and automatic cartesian partitioning methods
    • Benoit C., Jeanfaivre J. (2003). Three-Dimensional Inviscid Isolated Rotor Calculations Using Chimera and Automatic Cartesian Partitioning Methods, J. of the American Helicopter Society, 48, 128-138.
    • (2003) J. of the American Helicopter Society , vol.48 , pp. 128-138
    • Benoit, C.1    Jeanfaivre, J.2
  • 16
    • 33746624144 scopus 로고    scopus 로고
    • Application of cartesian background grid in combination with chimera method to predict aerodynamics of helicopter fuselage
    • Friedrichshafen, Germany
    • th European Rotorcraft Forum, Friedrichshafen, Germany.
    • (2003) th European Rotorcraft Forum
    • Khier, W.1    Schwarz, T.2
  • 20
    • 2942757053 scopus 로고
    • Approximate riemann solvers, parameter vectors and difference schemes
    • Roe P.L. (1981). Approximate Riemann Solvers, Parameter Vectors and Difference Schemes, Journal of Computational Physics, 43, 357-372.
    • (1981) Journal of Computational Physics , vol.43 , pp. 357-372
    • Roe, P.L.1
  • 22
    • 0038165706 scopus 로고    scopus 로고
    • Method of weakest descent for automatic block merging
    • th International Conference on Numerical methods in Fluid Dynamics, Springer
    • th International Conference on Numerical methods in Fluid Dynamics, Lecture Notes in Physics, Springer, 522-527.
    • (1996) Lecture Notes in Physics , pp. 522-527
    • Rigby, D.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.