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Volumn 36, Issue 5, 1999, Pages 769-776

Hybrid airfoil design procedure validation for full-scale ice accretion simulation

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ICE PROBLEMS; TRANSPORT AIRCRAFT; WIND TUNNELS;

EID: 0033360708     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2532     Document Type: Article
Times cited : (30)

References (22)
  • 4
  • 11
    • 0021466714 scopus 로고
    • Effect of geometry on airfoil icing characteristics
    • Bragg, M. B., "Effect of Geometry on Airfoil Icing Characteristics," Journal of Aircraft, Vol. 21, No. 7, 1984, pp. 505-511.
    • (1984) Journal of Aircraft , vol.21 , Issue.7 , pp. 505-511
    • Bragg, M.B.1
  • 13
    • 0030853037 scopus 로고    scopus 로고
    • Design of subscale airfoils with full-scale leading edges for ice accretion testing
    • also AIAA Paper 96-0635, Jan. 1996
    • Saeed, F., Selig, M. S., and Bragg, M. B., "Design of Subscale Airfoils with Full-Scale Leading Edges for Ice Accretion Testing," Journal of Aircraft, Vol. 34, No. 1, 1997, pp. 94-100; also AIAA Paper 96-0635, Jan. 1996.
    • (1997) Journal of Aircraft , vol.34 , Issue.1 , pp. 94-100
    • Saeed, F.1    Selig, M.S.2    Bragg, M.B.3
  • 14
    • 0343425184 scopus 로고
    • Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering, Ohio State Univ., Columbus, OH, 1981; also NASA CR 165599, March
    • Bragg, M. B., "Rime Ice Accretion and Its Effect on Airfoil Performance," Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering, Ohio State Univ., Columbus, OH, 1981; also NASA CR 165599, March 1982.
    • (1982) Rime Ice Accretion and Its Effect on Airfoil Performance
    • Bragg, M.B.1
  • 15
    • 0024552399 scopus 로고
    • XFOIL: An analysis and design system for low reynolds number airfoils
    • edited by T. J. Mueller, Springer-Verlag, New York
    • Drela, M., "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils," Lecture Notes in Engineering: Low Reynolds Number Aerodynamics, edited by T. J. Mueller, Vol. 54, Springer-Verlag, New York, 1989, pp. 1-12.
    • (1989) Lecture Notes in Engineering: Low Reynolds Number Aerodynamics , vol.54 , pp. 1-12
    • Drela, M.1
  • 16
    • 0026864308 scopus 로고
    • A multipoint inverse airfoil design method based on conformal mapping
    • Selig, M. S., and Maughmer, M. D., "A Multipoint Inverse Airfoil Design Method Based on Conformal Mapping," AIAA Journal, Vol. 30, No. 5, 1992, pp. 1162-1170.
    • (1992) AIAA Journal , vol.30 , Issue.5 , pp. 1162-1170
    • Selig, M.S.1    Maughmer, M.D.2
  • 17
    • 0032026779 scopus 로고    scopus 로고
    • Hybrid airfoil design method to simulate full-scale ice accretion throughout a given a range
    • also AIAA Paper 97-0054, Jan. 1997
    • Saeed, F., Selig, M. S., and Bragg, M. B., "Hybrid Airfoil Design Method to Simulate Full-Scale Ice Accretion Throughout a Given a Range," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 233-239; also AIAA Paper 97-0054, Jan. 1997.
    • (1998) Journal of Aircraft , vol.35 , Issue.2 , pp. 233-239
    • Saeed, F.1    Selig, M.S.2    Bragg, M.B.3
  • 18
    • 0343425182 scopus 로고    scopus 로고
    • Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering, Univ. of Illinois at Urbana-Champaign, Urbana, IL, Jan.
    • Saeed, F., "Hybrid Airfoil Design Methods for Full-Scale Ice Accretion Simulation," Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering, Univ. of Illinois at Urbana-Champaign, Urbana, IL, Jan. 1999.
    • (1999) Hybrid Airfoil Design Methods for Full-scale Ice Accretion Simulation
    • Saeed, F.1
  • 22
    • 0028496816 scopus 로고
    • Repeatability of ice shapes in the NASA lewis icing research tunnel
    • Shin, J., and Bond, T. H., "Repeatability of Ice Shapes in the NASA Lewis Icing Research Tunnel," Journal of Aircraft, Vol. 31, No. 5, 1994, pp. 1057-1063.
    • (1994) Journal of Aircraft , vol.31 , Issue.5 , pp. 1057-1063
    • Shin, J.1    Bond, T.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.