Investigation of Supersonic Free Jets Emanating from Convergent - Divergent Nozzles

Author:

MEHTA R. C.,PRASAD J. K.

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Reference13 articles.

1. A NOTE ON PRANDTL'S FORMULA FOR THE WAVE-LENGTH OF A SUPERSONIC GAS JET

2. Love , E. S. , Grigsby , C. E. , Lee , L. P. and Woodling , M. J. ( 1959 ). Experimental and theoretical studies of axisym-metric free jets , NASA TR-6

3. Shock associated noise of supersonic jets from convergent-divergent nozzles

4. Analysis of turbulent underexpanded jets. II - Shock noise features using SCIPVIS

5. Harper-Bourne , M. and Fisher , M. J. ( 1973 ). The noise from shock wave in supersonic jets , AGARD CP-131 , 1–13 .

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