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Volumn 1, Issue , 2004, Pages 247-262

Validation of inlet and exhaust boundary conditions for a cartesian method

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY CONDITIONS; COMPUTER AIDED DESIGN; COMPUTER SIMULATION; INTAKE SYSTEMS; MATHEMATICAL MODELS; NOZZLES; VISCOUS FLOW;

EID: 20744431576     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4837     Document Type: Conference Paper
Times cited : (10)

References (16)
  • 1
    • 20744450703 scopus 로고    scopus 로고
    • Simulation of transonic viscous flow over a fighter-like configuration including inlet
    • Flores, J., Chaderjian, N., and Sorenson, R., "Simulation of Transonic Viscous Flow over a Fighter-like Configuration Including Inlet," AIAA paper 87-1199.
    • AIAA Paper , vol.87 , Issue.1199
    • Flores, J.1    Chaderjian, N.2    Sorenson, R.3
  • 2
    • 20744456545 scopus 로고
    • Jet-induced flow separation on a lifting entry body at mach number from 4.00 to 6.00
    • NASA Langley Research Center, April
    • McGhee, R. J., "Jet-Induced Flow Separation on a Lifting Entry Body at Mach Number from 4.00 to 6.00," NASA Technical Memorandum NASA TM X-1997, NASA Langley Research Center, April 1970.
    • (1970) NASA Technical Memorandum , vol.NASA TM X-1997
    • McGhee, R.J.1
  • 3
    • 2942724228 scopus 로고    scopus 로고
    • Computational study of axisymmetric off-design nozzle flows
    • DalBello, T., Georgiadis, N. J., Yoder, D. A., and Keith, T. G., "Computational Study of Axisymmetric Off-design Nozzle Flows," AIAA paper 2004-0530.
    • AIAA Paper , vol.2004 , Issue.530
    • Dalbello, T.1    Georgiadis, N.J.2    Yoder, D.A.3    Keith, T.G.4
  • 4
    • 1842721928 scopus 로고    scopus 로고
    • Robust and efficient Cartesian mesh generation for component-based geometry
    • Aftosmis, M. J., Berger, M. J., and Melton, J. E., "Robust and efficient Cartesian mesh generation for component-based geometry," AIAA Paper 97-0196.
    • AIAA Paper , vol.97 , Issue.196
    • Aftosmis, M.J.1    Berger, M.J.2    Melton, J.E.3
  • 5
    • 0003258046 scopus 로고    scopus 로고
    • A parallel multilevel method for adaptively refined cartesian grids with embedded boundaries
    • Aftosmis, M. J., Berger, M. J., and Adomovicius, G., "A parallel multilevel method for adaptively refined Cartesian grids with embedded boundaries," AIAA Paper 2000-0808.
    • AIAA Paper , vol.2000 , Issue.808
    • Aftosmis, M.J.1    Berger, M.J.2    Adomovicius, G.3
  • 7
    • 20744433165 scopus 로고    scopus 로고
    • Base flow / underexpanded exhaust plume interaction in a supersonic external flow
    • Bannink, W. J., Houtman, E. M., and Bakker, P. G., "Base Flow / Underexpanded Exhaust Plume Interaction in a Supersonic External Flow," AIAA paper 98-1598.
    • AIAA Paper , vol.98 , Issue.1598
    • Bannink, W.J.1    Houtman, E.M.2    Bakker, P.G.3
  • 8
    • 0013400197 scopus 로고
    • An investigation of the effectiveness of several devices in simulating a rocket plume at free stream mach numbers of 0.9 to 1.2
    • U. S. Army Missile Command. Redstone Arsenal, Alabama, September
    • Burt, J. R., "An Investigation of the Effectiveness of Several Devices in Simulating a Rocket Plume at Free Stream Mach Numbers of 0.9 to 1.2," Tech. Rep. RD-TR-71-22, U. S. Army Missile Command. Redstone Arsenal, Alabama, September 1971.
    • (1971) Tech. Rep. , vol.RD-TR-71-22
    • Burt, J.R.1
  • 9
    • 0003432880 scopus 로고
    • Equations, tables, and charts for compressible flow
    • Ames Aeronautical Laboratory, Moffett Field, CA
    • Staff, A. R., "Equations, Tables, and Charts for Compressible Flow," Tech. rep., Ames Aeronautical Laboratory, Moffett Field, CA, 1953.
    • (1953) Tech. Rep.
    • Staff, A.R.1
  • 10
    • 0025502624 scopus 로고
    • Numerical simulation of an F-16A at angle of attack
    • October
    • Huband, G. W., Shang, J. S., and Aftosmis, M. J., "Numerical Simulation of an F-16A at Angle of Attack," J. of Aircraft, Vol. 27, No. 10, October 1990, pp. 886-892.
    • (1990) J. of Aircraft , vol.27 , Issue.10 , pp. 886-892
    • Huband, G.W.1    Shang, J.S.2    Aftosmis, M.J.3
  • 12
    • 20744460856 scopus 로고    scopus 로고
    • Experimental and computational comparison of an underexpanded jet flowfield
    • McDaniel, J. C. J., Glass, C. E., Staack, D., and Miller. C. G. I., "Experimental and Computational Comparison of an Underexpanded Jet Flowfield," AIAA Paper 2002-0305.
    • AIAA Paper , vol.2002 , Issue.305
    • McDaniel, J.C.J.1    Glass, C.E.2    Staack, D.3    Miller, C.G.I.4
  • 13
    • 0002369990 scopus 로고
    • The structure and utilization of supersonic free jets in low density wind tunnels
    • Rarefied Gas Dynamics, edited by J. H. de Leeuw, Academic Press. Section 7: Experimental Methods in Rarefied Gas Dynamics
    • Ashkenas, H. and Sherman, F., "The Structure and Utilization of Supersonic Free Jets in Low Density Wind Tunnels," Rarefied Gas Dynamics, edited by J. H. de Leeuw, Vol. II, Supplement 3 of Advances in Applied Mechanics, Academic Press, 1966, pp. 84-105. Section 7: Experimental Methods in Rarefied Gas Dynamics.
    • (1966) Advances in Applied Mechanics , vol.2 , Issue.3 SUPPL. , pp. 84-105
    • Ashkenas, H.1    Sherman, F.2
  • 15
    • 20744457026 scopus 로고    scopus 로고
    • D'Agostino, M., Marshall Space Flight Center, NASA, Huntsville, AL, Private communication
    • D'Agostino, M., Marshall Space Flight Center, NASA, Huntsville, AL, Private communication.
  • 16
    • 20744448162 scopus 로고    scopus 로고
    • Parameter studies using a cartesian method
    • Murman, S., Aftosmis, A., and Nemec, M., "Parameter Studies Using a Cartesian Method," AIAA paper 2004-5076.
    • AIAA Paper , vol.2004 , Issue.5076
    • Murman, S.1    Aftosmis, A.2    Nemec, M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.