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Volumn , Issue , 2000, Pages

Unsteady separated flow simulations using a cluster of workstations

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BENCHMARKING; COST EFFECTIVENESS; COST ENGINEERING; FLOW SIMULATION; NASA; SUPERCOMPUTERS;

EID: 85089110474     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-272     Document Type: Conference Paper
Times cited : (13)

References (25)
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  • 3
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    • Wind Tunnel Measurements of Ship Induced Turbulence and the Prediction of Helicopter Rotor Blade Response
    • Hurst, D. W. and Newman, S., "Wind Tunnel Measurements of Ship Induced Turbulence and the Prediction of Helicopter Rotor Blade Response, " Vertica, Vol. 12, No. 3, 1988, pp. 267-278.
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    • Hurst, D.W.1    Newman, S.2
  • 5
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    • Dynamic Interface Testing and the Pilots Rating Scale
    • Apr
    • Williams, S. and Long, K. R., "Dynamic Interface Testing and the Pilots Rating Scale, " The 53rd AHS Forum, Apr. 1997.
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    • Williams, S.1    Long, K.R.2
  • 8
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    • Progress Toward a User-Oriented Unstructured Viscous Grid Generator
    • Jan
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    • Pirzadeh, S.1
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    • Molecular Dynamics Simulation of Dissociation Kinetics
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    • (2000) AIAA Paper 2000-0213
    • Kantor, A.1    Long, L.N.2    Micci, M.M.3
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    • Higher Order Accurate Methods for Vortex Flow Simluations
    • May
    • Hall, C. M. and Long, L. N., "Higher Order Accurate Methods for Vortex Flow Simluations, " AHS Forum, Montreal, Canada, May 1999.
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    • Hall, C.M.1    Long, L.N.2
  • 18
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    • The Prospects for Simulating the Helicopter/Ship Interface
    • Mar
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.