Numerical investigation of transonic resonance with a convergent-divergent nozzle

AIAA Journal

Volumn 40, Issue 12, 2002, Pages 2393-2401

  Loh, Ching Y ^a   Zaman, K B M Q ^b  

^a Taitech Inc   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; BOUNDARY CONDITIONS; CALCULATIONS; NAVIER STOKES EQUATIONS; NOZZLES; OSCILLATIONS; PRESSURE; RESONANCE; SHOCK WAVES; TRANSONIC AERODYNAMICS; UNSTEADY FLOW;

CONSERVATION ELEMENT AND SOLUTION ELEMENT METHOD; CONVERGENT DIVERGENT NOZZLE; PRESSURE RATIO; TRANSONIC RESONANCE;

AEROSPACE ENGINEERING;

EID: 0036942297     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1607     Document Type: Article

References (15)

1. Zaman, K. B. M. Q., Dahl, M. D., Bencic, T. J., and Loh, C. Y., "Experimental Investigation of 'Transonic Resonance' with Convergent-Divergent Nozzles," Journal of Fluid Mechanics, Vol. 463, 2002, pp. 313-343.
2. Loh, C. Y., Hultgren, L. S., and Chang S.-C., "Computing Waves in Compressible Flow Using the Space-Time Conservation Element Solution Element Method," AIAA Journal, Vol. 39, No. 5, 2001, pp. 794-801; also AIAA Paper 98-0369, 1998.
3. Chang, S. C., "The Method of Space-Time Conservation Element and Solution Element-A New Approach for Solving the Navier-Stokes and Euler Equations," Journal of Computational Physics, Vol. 119, 1995, pp. 295-324.
4. Chang, S.-C., Wang, X.-Y., and Chow, C.-Y., "The Space-Time Conservation Element and Solution Element Method-A New High Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws," Journal of Computational Physics, Vol. 159, 1999, pp. 89-136.
5. Wang, X.-Y., and Chang, S.-C., "A 2-D Non-splitting Unstructured Triangular Mesh Euler Solver Based on the Space-Time Conservation Element and Solution Element Method," Computational Fluid Dynamics Journal, Vol. 8, 1999, pp. 309-325.
6. Loh, C. Y., Hultgren, L. S., Chang, S.-C., and Jorgenson, P.C. E., "Vortex Dynamics Simulation in Aeroacoustics by the Space-Time Conservation Element Solution Element Method," AIAA Paper 99-0359, Jan. 1999.
7. Loh, C. Y., Hultgren, L. S., and Jorgenson, P. C. E., "Near Field Screech Noise Computation for an Underexpanded Supersonic Jet by the CE/SE Method," AIAA Paper 2001-2252, May 2001.
8. Chang, S.-C., Himansu, A., Loh, C. Y., Wang, X. Y., Yu, S.-T., and Jorgenson, P. C. E., "Robust and Simple Non-Reflecting Boundary Conditions for the Space-Time Conservation Element and Solution Element Method," AIAA Paper 97-2077, July 1997.
9. Bogey, C., Bailly, C., and Juvé D., "Computation of the Sound Radiated by a 3-D Jet Using Large Eddy Simulation," AIAA Paper 2000-2009, June 2000.
10. Hunter, C. A., "Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows," AIAA Paper 98-3107, July 1998.
11. Ishibashi, M., and Takamoto, M., "Discharge Coefficients of Critical Nozzles with Step Near the Throat and Their Flow Field Estimated from Recovery Temperature Distribution," American Society of Mechanical Engineers, Fluids Engineering Div. Summer Meeting, ASME Paper FED-SM2001-18035, May 2001.
12. Hu, F. Q., and Manthey, J. L., "Application of PML Absorbing Boundary Conditions to the Benchmark Problems of Computational Aeroacoustics," Second CAA Workshop on Benchmark Problems, edited by C. K. W. Tam and J. C. Hardin, NASA CP-3352, June 1997.
13. Hsieh, T., and Coakley, T. J., "Downstream Boundary Effects on Frequency of Self-Excited Oscillations in Transonic Diffuser Flows," AIAA Paper 87-0161, Jan. 1987.
14. Bogar, T. J., Sajben, M., and Kroutil, J. C., "Characteristic Frequencies of Transonic Diffuser Flow Oscillations," AIAA Journal, Vol. 21, No. 9, 1983, pp. 1232-1240.
15. von Lavante, E., Zaichcial, A., Nath, B., and Dietrich, H., "Numerical and Experimental Investigation of Unsteady Effects in Critical Venturi Nozzles," Flow Measurement and Instrumentation, Vol. 11, 2000, pp. 257-264.