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Volumn 3, Issue , 2004, Pages 1431-1441

3d-duct design using variable fidelity method

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AUTOMATION; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FIGHTER AIRCRAFT; NAVIER STOKES EQUATIONS; OPTIMIZATION;

EID: 20344378460     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4427     Document Type: Conference Paper
Times cited : (11)

References (21)
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    • Harloff, G. J., Smith, C. P., Bruns, J. E., and DeBonis, J. R., "Navier-Slokes Analysis of three dimensional S-ducts," Journal of Aircraft, Vol. 30, No. 4. July-Aug. 1993.
    • (1993) Journal of Aircraft , vol.30 , Issue.4
    • Harloff, G.J.1    Smith, C.P.2    Bruns, J.E.3    DeBonis, J.R.4
  • 5
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    • Modeling of subsonic flow through a Compact Offset Inlet diffuser
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    • Jenkins, R. C., and Loeffler Jr., A. L., "Modeling of subsonic flow through a Compact Offset Inlet diffuser," AIAA Journal, Vol. 29, No. 3, March 1991.
    • (1991) AIAA Journal , vol.29 , Issue.3
    • Jenkins, R.C.1    Loeffler Jr., A.L.2
  • 7
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    • A synthesis of procedures for selecting the geometric features of an air intake for M=0 to 1.8
    • November
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    • User's guide for FFSQP version 3.7: A fortran code for solving optimization programs, possibly minimax, with general inequality constraints and linear equality constraints, generating feasible iterates
    • Univ. of Maryland, Technical Report SRC-TR-92-1075, College Park, MD
    • Zhou, J. L., Tits, A. L. and Lawrence, C. T., "User's Guide for FFSQP Version 3.7: A Fortran Code for Solving Optimization Programs, Possibly Minimax, with General Inequality Constraints and Linear Equality Constraints, Generating Feasible Iterates," Institute for Systems Research, Univ. of Maryland, Technical Report SRC-TR-92-1075, College Park, MD, 1997. (http://www.aemdesign.com/)
    • (1997) Institute for Systems Research
    • Zhou, J.L.1    Tits, A.L.2    Lawrence, C.T.3
  • 13
    • 85088342990 scopus 로고    scopus 로고
    • Computation of three dimensional compressible turbulent flow through a non-diffusing S-duct
    • CFD Division, Aeronautical Society of India, Bangalore, 9-10 August
    • th Annual CFD Symposium, CFD Division, Aeronautical Society of India, Bangalore, 9-10 August, 2002.
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  • 14
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    • A New k-ε eddy viscosity model for high Reynolds number turbulent flows
    • Shih, T. H., Liou, W. W., Shabbir, A., Yang, Z., and Zhu, J., "A New k-ε eddy viscosity model for high Reynolds number turbulent flows," Computers & Fluids, Vol. 24, No. 3, pp. 227-238.
    • Computers & Fluids , vol.24 , Issue.3 , pp. 227-238
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  • 16
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    • Automated design optimization of a three-dimensional S-shaped subsonic diffuser
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    • Lefantzi, S., and Knight, D. D., "Automated design optimization of a three-dimensional S-shaped subsonic diffuser," J. of Propulsion & Power, Vol. 18, No. 4, July-August 2002.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.