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Volumn , Issue , 1997, Pages 1-16

Design of efficient Go2/GH2 injectors: A NASA, industry and university cooperative effort

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE INDUSTRY; APPLICATION PROGRAMS; COMPUTATION THEORY; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE REUSABILITY; CRASHWORTHINESS; FLAMMABILITY TESTING; NASA; PROPULSION; REUSABILITY; ROCKET ENGINES; ROCKETS; SPACE FLIGHT;

EID: 84962883027     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (23)
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  • 8
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    • Compressible and Incompressible Flow Computations With a Pressure Based Method
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    • Chen, Y.S.1
  • 10
    • 0029427240 scopus 로고
    • A Unified Two-Phase Numerical Method for General Gas-Liquid Flow Applications
    • GL-19, Hilton Head, SC, August
    • Chen, Y.-S., Shang H.-M, Liaw, P, Chen, C.-P and Wang T.-S., “A Unified Two-Phase Numerical Method for General Gas-Liquid Flow Applications,” 1995 ASME Summer Meeting, GL-19, Hilton Head, SC, August, 1995
    • (1995) 1995 ASME Summer Meeting
    • Chen, Y.-S.1    Shang, H.-M.2    Liaw, P.3    Chen, C.-P.4    Wang, T.-S.5
  • 13
    • 0028465044 scopus 로고
    • Hot Gas-Side Heat Transfer in Liquid Rocket Engine Combustors
    • July-Sept
    • Wang, T.-S., and Luong, V., “Hot Gas-Side Heat Transfer in Liquid Rocket Engine Combustors,” Journal of Thermophysics and Heat Transfer. Vol. 8, No. 3, July-Sept., 1994, pp. 524-530.
    • (1994) Journal of Thermophysics and Heat Transfer , vol.8 , Issue.3 , pp. 524-530
    • Wang, T.-S.1    Luong, V.2
  • 14
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    • Numerical Study of the Transient Nozzle Flow Separation of Liquid Rocket Engines
    • October
    • Wang, T.-S., “Numerical Study of the Transient Nozzle Flow Separation of Liquid Rocket Engines,” Computational Fluid Dynamics Journal. Vol. 1, No. 3, October, 1992, pp. 319-328.
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    • Wang, T.-S.1
  • 15
    • 84963908031 scopus 로고
    • Axisymmetric Computational Fluid Dynamics Analysis of a Film/Dump-Cooled Rocket Nozzle Plume
    • June 28-30, Monterey, CA
    • Tucker, P. K., and Warsi, S. A., “Axisymmetric Computational Fluid Dynamics Analysis of a Film/Dump-Cooled Rocket Nozzle Plume,” AIAA 93-2349, 29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, June 28-30, 1993, Monterey, CA.
    • (1993) AIAA 93-2349, 29Th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
    • Tucker, P.K.1    Warsi, S.A.2
  • 16
    • 0029376218 scopus 로고
    • Numerical Analysis of Base Flovvfield for a Four-Engine Clustered Nozzle Configuration
    • September-October
    • Wang, T.-S., “Numerical Analysis of Base Flovvfield for a Four-Engine Clustered Nozzle Configuration,” Journal of Propulsion and Power. Vol. 11, No. 5, September-October, 1995, pp. 1076-1078.
    • (1995) Journal of Propulsion and Power , vol.11 , Issue.5 , pp. 1076-1078
    • Wang, T.-S.1
  • 17
    • 0029679057 scopus 로고    scopus 로고
    • Grid-Resolved Analysis of a Four-Engine Clustered Nozzle Configuration
    • January-February
    • Wang T.-S., “Grid-Resolved Analysis of a Four-Engine Clustered Nozzle Configuration,” Journal of Spacecraft and Rockets. Vol. 33, No. 1, January-February, 1996, pp. 22-29.
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.1 , pp. 22-29
    • Wang, T.-S.1
  • 18
    • 0030149176 scopus 로고    scopus 로고
    • Computational Pollutant Environment Assessment from Propulsion System Testing
    • May- June
    • Wang, T.-S., McConnaughey, P. K., Warsi, S. A., and Chen, Y.-S., “Computational Pollutant Environment Assessment from Propulsion System Testing,” Journal of Spacecraft and Rockets. Vol. 33, No. 3, May- June, 1996, pp. 386-392.
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.3 , pp. 386-392
    • Wang, T.-S.1    MCConnaughey, P.K.2    Warsi, S.A.3    Chen, Y.-S.4
  • 19
    • 0000154992 scopus 로고    scopus 로고
    • Shear Coaxial Injector Atomization Phenomena For Combustion and Non-Combusting Conditions
    • Pal, S., Moser, M. D., Ryan, H. M., Foust, M. J., and Santoro, R. J., “Shear Coaxial Injector Atomization Phenomena For Combustion and Non-Combusting Conditions”, Atomization and Sprays. Vol. 6, pp. 227-244, 1996.
    • (1996) Atomization and Sprays , vol.6 , pp. 227-244
    • Pal, S.1    Moser, M.D.2    Ryan, H.M.3    Foust, M.J.4    Santoro, R.J.5
  • 20
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    • Atomization Characteristics Of Impinging Liquid Jets
    • January-February
    • Ryan, H. M., Anderson, W. E., Pal, S. and Santoro, R. J., “Atomization Characteristics Of Impinging Liquid Jets,” Journal of Propulsion and Power. Vol. 11, No. 1, pp. 135-145, January-February 1995.
    • (1995) Journal of Propulsion and Power , vol.11 , Issue.1 , pp. 135-145
    • Ryan, H.M.1    Erson, W.E.2    Pal, S.3    Santoro, R.J.4
  • 22
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    • Liquid-Film Properties for Centrifugal Spray Nozzles
    • October
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    • Doumas, M.1    Laster, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.