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Volumn , Issue , 2004, Pages

Performance trade-off studies for a retrofit Hybrid Laminar Flow Control System

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONFIGURATIONS; AIRCRAFT DRAG; DIRECT CONTROL; HYBRID LAMINAR FLOW CONTROLS; MASS FLOW RATE; PERFORMANCE TRADE-OFF; SUCTION SYSTEM; WING GEOMETRY;

EID: 84897806480     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (14)
  • 2
    • 84897816130 scopus 로고    scopus 로고
    • New Aerodynamic Approach to Suction System Design
    • Notes on Numerical Fluid Mechanics, edited by P. Thiede, Springer, Berlin
    • Atkin, C. J., "New Aerodynamic Approach to Suction System Design", Aerodynamic Drag Reduction Technologies, Notes on Numerical Fluid Mechanics, Vol. 76, edited by P. Thiede, Springer, Berlin, 2001, pp. 55-63.
    • (2001) Aerodynamic Drag Reduction Technologies , vol.76 , pp. 55-63
    • Atkin, C.J.1
  • 3
    • 84884927654 scopus 로고    scopus 로고
    • Predicting the cruise performance of a retrofit Hybrid Laminar Flow Control system
    • Cambridge, United Kingdom, June
    • Atkin, C. J., and Courtenay W. J. A., "Predicting the cruise performance of a retrofit Hybrid Laminar Flow Control system", CEAS Aerodynamics Conference, Cambridge, United Kingdom, June 2002.
    • (2002) CEAS Aerodynamics Conference
    • Atkin, C.J.1    Courtenay, W.J.A.2
  • 5
    • 0029406661 scopus 로고
    • Computation of compressible, laminar boundary layers on swept, tapered wings
    • Horton, H. P., and Stock, H. W. "Computation of compressible, laminar boundary layers on swept, tapered wings", J Aircraft, Vol. 32, No. 6, 1995, pp. 1402-1405.
    • (1995) J Aircraft , vol.32 , Issue.6 , pp. 1402-1405
    • Horton, H.P.1    Stock, H.W.2
  • 6
    • 84884957076 scopus 로고    scopus 로고
    • Correlation between linear stability analysis and crossflow transition near an attachment line
    • edited by R.A.W.M. Henkes and J.L. van Ingen, North-Holland, Amsterdam
    • Atkin, C. J., and Poll, D. I. A., "Correlation between linear stability analysis and crossflow transition near an attachment line", Transitional Boundary Layers in Aeronautics, edited by R.A.W.M. Henkes and J.L. van Ingen, North-Holland, Amsterdam, 1996, pp. 155-164.
    • (1996) Transitional Boundary Layers In Aeronautics , pp. 155-164
    • Atkin, C.J.1    Poll, D.I.A.2
  • 12
    • 84892820596 scopus 로고    scopus 로고
    • Parabolized stability equations and transition prediction for compressible swept-wing flows
    • November
    • Mughal, M. S., and Hall, P., "Parabolized stability equations and transition prediction for compressible swept-wing flows", Imperial College Report, November 1996.
    • (1996) Imperial College Report
    • Mughal, M.S.1    Hall, P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.