Interface wavelength between confined supersonic two-dimensional jets and subsonic streams

AIAA Journal

Volumn 35, Issue 7, 1997, Pages 1219-1221

  De Chant, Lawrence J ^a,b   Caton, Jerald A ^a,b,c   Andrews, Malcolm J ^a,b,c  

^a TEXAS A AND M UNIVERSITY   (United States)

^b MS 3123 ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 3242817298     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.218     Document Type: Article

References (7)

1. Champagne, G. A., "Jet Noise Reduction Concepts for the Supersonic Transport," AIAA Paper 91-3328, Sept. 1991.
2. De Chant, L. J., Seidel, J. A., and Andrews, M. J., "Interface Wavelength Between Supersonic Jets and Subsonic Flowfields," AIAA Journal, Vol. 34, No. 9, 1996, pp. 1946-1948.
3. Fabri, J., and Siestrunck, R., "Supersonic Air Ejectors," Advances in Applied Mechanics, Vol. 5, Academic, New York, pp. 1-34.
4. Addy, A. L., Dutton, J. C., and Mikkelsen, C. D., "Supersonic Ejector-Diffuser Theory and Experiments," Dept. of Mechanical and Industrial Engineering, Engineering Experiment Station, Univ. of Illinois, UILU-ENG-82-400, Urbana, IL, Aug. 1981.
5. Anderson, J. D., Modern Compressible Flow, McGraw-Hill, New York, pp. 120-128.
6. Burden, R. L., and Faires, J. D., Numerical Analysis, PWS-Kent, Boston, 1993, pp. 560-566.
7. De Chant, L. J., and Caton, J. A., "Measurement of Confined Supersonic, 2-d Jet Lengths Using the Hydraulic Analogy," Experiments in Fluids (submitted for publication).