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Volumn , Issue , 2013, Pages

Swept-wing ice accretion characterization and aerodynamics

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EXPERIMENTS; AERODYNAMIC TESTING; ATMOSPHERIC WIND TUNNEL; COLLABORATIVE RESEARCH; COMPUTATIONAL SIMULATION; TECHNICAL CHALLENGES; THREE-DIMENSIONAL MEASUREMENTS; UNIVERSITY OF ILLINOIS;

EID: 84883476918     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2013-2824     Document Type: Conference Paper
Times cited : (57)

References (61)
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  • 15
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    • Effect of High-Fidelity Ice-Accretion Simulations on Full-Scale Airfoil Performance
    • Jan.-Feb
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    • Jan-Feb
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    • Vargas, M.1
  • 20
    • 77958191303 scopus 로고    scopus 로고
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    • Seville, Spain, Paper No. 2007-01-3332
    • Vargas, M., "Swept Wing Icing Studies at NASA Glenn Research Center 1996-2006, " SAE Aircraft & Engine Icing International Conference, Seville, Spain, 2007, Paper No. 2007-01-3332.
    • (2007) SAE Aircraft & Engine Icing International Conference
    • Vargas, M.1
  • 55
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    • Hybrid Airfoil Design Procedure Validation for Full-Scale Ice Accretion Simulation
    • Sept.-Oct
    • Saeed, F., Selig, M. S., and Bragg, M. B., "Hybrid Airfoil Design Procedure Validation for Full-Scale Ice Accretion Simulation, " Journal of Aircraft, Vol. 36, No. 5, Sept.-Oct., 1999, pp. 769-776.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.