Improved two-dimensional dynamic stall prediction with structured and hybrid numerical methods

Annual Forum Proceedings - AHS International

Volumn 3, Issue , 2009, Pages 2434-2450

  Richter, K ^a   Le Pape, A ^b   Knopp, T ^a   Costes, M ^b   Gleize, V ^a   Gardner, A D ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER TRANSITIONS; DYNAMIC STALLS; EXPERIMENTAL DATA; HIGH-SPEED CONDITIONS; HYBRID NUMERICAL METHOD; LOW SPEED; NUMERICAL DYNAMICS; ONE-EQUATION; PITCHING AIRFOILS; REYNOLDS STRESS MODELS; ROTOR BLADES; SPALART-ALLMARAS; SPATIAL DISCRETIZATIONS; TEMPORAL RESOLUTION; TEST CASE; TURBULENCE MODELING;

AIRFOILS; ATMOSPHERIC THERMODYNAMICS; NUMBER THEORY; REYNOLDS NUMBER; SIMULATORS; TURBULENCE; TURBULENCE MODELS; TWO DIMENSIONAL; WALL FLOW;

NUMERICAL METHODS;

EID: 70449119309     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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