Computation of shock induced noise in imperfectly expanded supersonic jets

8th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Imamoglu, Bulent ^a   Balakumar, Ponnampalam ^b  

^a Old Dominion University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC JET; DISCRETIZATIONS; ESSENTIALLY NON-OSCILLATORY; INSTABILITY WAVES; SHOCK CELL STRUCTURE; SHOCK INDUCED; SHOCK-CELL; SUPERSONIC JETS;

ACOUSTIC NOISE; AEROACOUSTICS; LARGE EDDY SIMULATION; NAVIER STOKES EQUATIONS;

SUPERSONIC AERODYNAMICS;

EID: 84896884165     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Panda, J. "An Experimental Investigation of Screech Noise Generation", J. Fluid Mech., vol. 378, pp 71-96, 1999
2. Kim, J. W., Lee, D. J. "Generalized Characteristic Boundary Conditions for Computational Aeroacoustics", AIAA Journal, Vol. 38, No. 11, pp. 2040-2049, 2000
3. Loh, C. Y., Hultgren, L. S., Jorgenson, P. C. E., "Near Field Screech Noise Computation for an Underexpanded Supersonic Jet by the CE/SE Method", Paper Draft
4. Shen, H., Tam, C. K. W. "Numerical Simulation of the Generation of Axisymmetric Mode Jet Screech Tones", AIAA Journal, Vol. 36, No. 10, pp. 1801-1807, 1998
5. Shu, C. W. "Essentially Non-Oscillatory and Weighted Essentially Non-Oscillatory Schemes for Hyperbolic Conservation Laws", ICASE Report No. 97-65, 1997
6. Atkins, H. L., "High-Order ENO Methods for the Unsteady Compressible Navier-Stokes Equations", AIAA Paper 91-1557, 1991.