Interface wavelength between supersonic jets and subsonic flowfields

AIAA Journal

Volumn 34, Issue 9, 1996, Pages 1946-1948

  De Chant, Lawrence J ^a   Seidel, Jonathan A ^b   Andrews, Malcolm J ^a,c  

^a Department of Electrical and Computer Engineering   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

EID: 3242856133     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13331     Document Type: Article

References (8)

1. Champagne, G. A., "Jet Noise Reduction Concepts for the Supersonic Transport," AIAA Paper 91-3328, Sept. 1991.
2. Prandtl, L., "Ueber die stationaeren Wellen in einem Gasstrahle," Physik Z, Vol. 5, 1904, pp. 599-601.
3. Pai, S. I., "On Two-Dimensional Supersonic Flow of a Jet in Uniform Stream," Journal of the Aeronautical Sciences, Vol. 19, No. 1, 1952, pp. 61-65.
4. Pack, D. C., "A Note on Prandtl's Formula for the Wavelength of a Supersonic Gas Jet," Quarterly Journal of Mechanics and Applied Mathematics, Vol. 3, Pt. 2, 1950, pp. 173-181.
5. Love, E. S., Grigsby, C. E., Lee, L. P., and Woodling, M. J., "Experimental and Theoretical Studies of Axisymmetric FreeJets," NASA TR R-6, 1959.
6. Nayfeh, A., Perturbation Methods, Wiley, New York, 1973, pp. 57-109.
7. Lighthill, M. J., "A Technique for Reducing Approximate Solutions to Physical Problems Uniformly Valid," Zeitschrift für Flugwissenschaften, Vol.9, 1961, pp. 267-275.
8. Anderson, J. D., Modern Compressible Flow, McGraw-Hill, New York, 1982.