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Volumn 40, Issue 2, 2002, Pages 244-253

Unsteady flow evolution in porous chamber with surface mass injection, Part 2: Acoustic excitation

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE VELOCITY; BOUNDARY LAYERS; COMPUTER SIMULATION; CORRELATION METHODS; ENERGY TRANSFER; FLOW INTERACTIONS; HEAT TRANSFER COEFFICIENTS; LAMINAR FLOW; POROUS MATERIALS; SURFACE PROPERTIES; TURBULENT FLOW; VISCOSITY;

EID: 0036471743     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1666     Document Type: Article
Times cited : (62)

References (24)
  • 1
    • 0035421060 scopus 로고    scopus 로고
    • Unsteady flow evolution in a porous chamber with surface mass injection, Part 1: Free oscillation
    • (2001) AIAA Journal , vol.39 , Issue.8 , pp. 1577-1586
    • Apte, S.1    Yang, V.2
  • 14
    • 4243598920 scopus 로고    scopus 로고
    • Acoustically induced turbulent transition in solid propellant rocket chamber flowfields
    • AIAA Paper 99-2508
    • (1999)
    • Lee, Y.H.1    Beddini, R.A.2
  • 16
    • 0003777520 scopus 로고    scopus 로고
    • Unsteady flow evolution and combustion dynamics of homogeneous solid propellant in a rocket motor
    • Ph.D. Dissertation, Dept. of Mechanical and Nuclear Engineering, Pennsylvania State Univ., University Park, PA, July
    • (2000)
    • Apte, S.V.1
  • 18
    • 0003418258 scopus 로고
    • Numerical simulation of velocity-coupled combustion response of solid rocket propellants
    • Ph.D. Dissertation, Dept. of Mechanical Engineering, Pennsylvania State Univ., University Park, PA
    • (1992)
    • Tseng, I.S.1
  • 23
    • 85002656403 scopus 로고
    • Experimental investigation of rocket motor flow-turning acoustic losses
    • U.S. Air Force Rocket Propulsion Lab., TR-84-009, Edwards AFB, CA
    • (1984)
    • Hersch, A.S.1    Walker, B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.