Estimation of shock-cell structure of axisymmetric supersonic free jets

Indian Journal of Engineering and Materials Sciences

Volumn 3, Issue 4, 1996, Pages 141-147

  Mehta, R C ^a   Prasad, J K ^a  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0030359389     PISSN: 09714588     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

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9. Zeeuw D D & Powell K G, Euler calcualtions of axisymmetric under expanded jets by an adaptive-refinement method, AIAA paper 92-0321, 1992.
10. Jameson A, Schmidt W & Turkel E, Numerical simulation of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes, AIAA paper No. 81-1259, 1981.
11. Mehta R C & Prasad J K, Experimental and computational studies of high speed jet flows, Proc of the ASME/JSME, Fluid Engineering Annual Conference, USA, Aug. 13-18 (1995) 139-144.
12. Powell A, On the mechanism of choked jet noise, Proc Phys Soc, (London) Section B, 66 (1953) 1039-1056.
13. Harper-Bourno M & Fisher M J, The noise from shock waves in supersonic jets, in Noise Mechanisms, AGARD CP-131, AGARD, Neuilly-Sur-Seine, France (1973) 11.1-11.13.