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Volumn , Issue , 2000, Pages

Automated optimal design of supersonic and subsonic diffusers using CFD

Author keywords

Air intakes; Computational fluid dynamics; Inlets; Optimization; Subsonic diffusers; Supersonic diffusers

Indexed keywords

AUTOMATED DESIGN OPTIMIZATION; COMPUTATIONAL DESIGN; COMPUTER PERFORMANCE; INLETS; OPTIMAL PERFORMANCE; OPTIMIZATION ALGORITHMS; SUBSONIC DIFFUSERS; SUPERSONIC DIFFUSERS;

EID: 84893365355     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (29)
  • 3
    • 0031095642 scopus 로고    scopus 로고
    • Automated design optimization for the p2 and p8 hypersonic inlets
    • V. Shukla, A. Gelsey, M. Schwabacher, D. Smith and D. Knight, Automated Design Optimization for the P2 and P8 Hypersonic Inlets, AIAA Journal of Aircraft, Vol. 34, No. 2, pp. 228-235, (1997).
    • (1997) AIAA Journal of Aircraft , vol.34 , Issue.2 , pp. 228-235
    • Shukla, V.1    Gelsey, A.2    Schwabacher, M.3    Smith, D.4    Knight, D.5
  • 4
    • 0003997741 scopus 로고    scopus 로고
    • User's guide for CFSQP, a code for solving constrained nonlinear optimization problems, generating iterates satisfying all inequality constraints
    • University of Maryland
    • C. Lawrence, J. Zhou and A. Tits, User's Guide for CFSQP, A Code for Solving Constrained Nonlinear Optimization Problems, Generating Iterates Satisfying All Inequality Constraints, Report TR-94-16rl, Dept Electrical Engineering, University of Maryland, (1996).
    • (1996) Report TR-94-16rl, Dept Electrical Engineering
    • Lawrence, C.1    Zhou, J.2    Tits, A.3
  • 9
    • 0019999091 scopus 로고
    • Predictions of channel and boundary layer flows with a low reynolds number turbulence model
    • K. Chien, Predictions of Channel and Boundary Layer Flows with a Low Reynolds Number Turbulence Model, AIAA Journal Vol. 20, No. 1, pp. 33-38, (1982).
    • (1982) AIAA Journal , vol.20 , Issue.1 , pp. 33-38
    • Chien, K.1
  • 10
    • 0032208514 scopus 로고    scopus 로고
    • Automated optimal design of two dimensional supersonic missile inlets
    • M. Blaize, D. Knight and K. Rasheed, Automated Optimal Design of Two Dimensional Supersonic Missile Inlets, AIAA Journal of Propulsion and Power, Vol. 14, No. 6, pp. 890-898, (1998).
    • (1998) AIAA Journal of Propulsion and Power , vol.14 , Issue.6 , pp. 890-898
    • Blaize, M.1    Knight, D.2    Rasheed, K.3
  • 12
    • 84893355992 scopus 로고
    • Computation of supersonic intakes, AGARD special course on missile aerodynamics
    • R. Lacau, P. Ganero and F. Gaible, Computation of Supersonic Intakes, AGARD Special Course on Missile Aerodynamics, AGARD Report 804, (1994).
    • (1994) AGARD Report , pp. 804
    • Lacau, R.1    Ganero, P.2    Gaible, F.3
  • 20
    • 0029720269 scopus 로고    scopus 로고
    • Improving curved subsonic diffuser performance with vortex generators
    • B. Reichert and B. Wendt, Improving Curved Subsonic Diffuser Performance with Vortex Generators, AIAA Journal, Vol. 34, No. 1, pp. 65-72, (1996).
    • (1996) AIAA Journal , vol.34 , Issue.1 , pp. 65-72
    • Reichert, B.1    Wendt, B.2
  • 21
    • 0027592330 scopus 로고
    • Study on vortex generator flow control for the management of inlet distortion
    • B. Anderson and J. Gibb, Study on Vortex Generator Flow Control for the Management of Inlet Distortion, Journal of Propulsion and Power, Vol. 9, No. 3, pp. 422-430, (1993).
    • (1993) Journal of Propulsion and Power , vol.9 , Issue.3 , pp. 422-430
    • Anderson, B.1    Gibb, J.2
  • 29
    • 8344255241 scopus 로고
    • Navier-stokes analysis and experimental data comparison of compressible flow within ducts
    • G. Harloff, B. Reichert and J. Sirbaugh, Navier-Stokes Analysis and Experimental Data Comparison of Compressible Flow Within Ducts, NASA Technical Memorandum 105796, (1992).
    • (1992) NASA Technical Memorandum 105796
    • Harloff, G.1    Reichert, B.2    Sirbaugh, J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.