Computation of shock-sound interaction using finite volume essentially nonoscillatory scheme

AIAA Journal

Volumn 40, Issue 6, 2002, Pages 1239-1240

  Kim, Yong Seok ^a,b   Lee, Duck Joo ^a,b  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Gwangju Institute of Science and Technology   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; ALGORITHMS; APPROXIMATION THEORY; COMPUTATIONAL METHODS; FINITE VOLUME METHOD; INTERPOLATION;

CONVERGING DIVERGING NOZZLE; MODIFIED FLUX APPROACH; SHOCK SOUND INTERACTION;

SHOCK WAVES;

EID: 0036603033     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1779     Document Type: Article

References (8)

1. Essentially non-oscillatory methods for shock-sound interaction
2. Uniformly high-order accurate nonoscillatory schemes III
3. Computing unsteady shock waves for aeroacoustic applications
4. High-resolution, nonoscillatory schemes for unsteady compressible flows
5. Numerical analysis of internal combustion engine intake noise with a moving piston and a valve
6. High-order ENO methods for the unsteady Navier-Stokes equations
7. Using high-order accurate essentially nonoscillatory schemes for aeroacoustic applications
8. Transparent acoustic source condition applied to the Euler equations