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Volumn 7, Issue 6, 2003, Pages 465-472

Improvements on computations of high speed propeller unsteady aerodynamics

Author keywords

CFD computation; Propeller; Transonic flows; Turboprop aircraft; Unsteady flows; Wind tunnel test

Indexed keywords

AIRFRAMES; COMPUTATIONAL FLUID DYNAMICS; FLUID STRUCTURE INTERACTION; NAVIER STOKES EQUATIONS; STEADY FLOW; TRANSONIC FLOW; TRANSPORT AIRCRAFT; TURBOMACHINE BLADES; TURBOPROP ENGINES; UNSTEADY FLOW; VISCOSITY; WIND TUNNELS; WINGS;

EID: 0347985180     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(03)00046-4     Document Type: Article
Times cited : (44)

References (15)
  • 4
    • 0026886780 scopus 로고
    • Predicted pressure distribution on a prop-fan blade through Euler analysis
    • Kobayakawa M., et al. Predicted pressure distribution on a prop-fan blade through Euler analysis. AIAA J. Aircraft. 29:(4):1992.
    • (1992) AIAA J. Aircraft , vol.29 , Issue.4
    • Kobayakawa, M.1
  • 7
    • 0028425087 scopus 로고
    • Unsteady blade pressures on a Propfan: Predicted and measured compressibility effects
    • Nallasamy M. Unsteady blade pressures on a Propfan: predicted and measured compressibility effects. AIAA J. Aircraft. 31:(3):1994.
    • (1994) AIAA J. Aircraft , vol.31 , Issue.3
    • Nallasamy, M.1
  • 14
    • 0348196932 scopus 로고    scopus 로고
    • Wind tunnel tests and CFD predictions of the flow-field of a high-speed six-blades propeller in steady and unsteady conditions
    • Paper 18, Braunschweig, Germany
    • Averardo M.A., et al. Wind tunnel tests and CFD predictions of the flow-field of a high-speed six-blades propeller in steady and unsteady conditions. Workshopon EU-Research on Aerodynamic Engine/Aircraft Integration for Transport Aircraft, Paper 18, Braunschweig, Germany. 2000.
    • (2000) Workshopon EU-research on Aerodynamic Engine/Aircraft Integration for Transport Aircraft
    • Averardo, M.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.