Aeroacoustic boundary element method using analytical/numerical matching

AIAA Journal

Volumn 35, Issue 2, 1997, Pages 244-254

  Epstein, Ronald J ^a,b   Bliss, Donald B ^a,c  

^a DUKE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c Department of Mechnical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC TECHNIQUES; AERODYNAMICS; BOUNDARY ELEMENT METHODS;

EID: 0030934050     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.114     Document Type: Article

References (4)

1. Erickson, L. L., "Panel Methods - An Introduction," NASA TP 2995, 1990.
2. Lifanov, I. K., and Polonskii, I. E., "Proof of the Numerical Method of Discrete Vortices of Solving Singular Integral Equations," Journal of Applied Mathematics and Mechanics, Vol 39, No. 4, 1975, pp 742-746.
3. Johnson, F. T., and Rubbert, P. E., "Advanced Panel-Type Influence Coefficient Methods Applied to Subsonic Flows," AIAA Piper 75-50, Jan. 1975.
4. Johnson, F. T., Rubbert, P. E., and Ehlers, F. E., "A Higher Order Panel Method for General Analysis and Design Applications in Subsonic Flow," 5th International Conference on Numerical Methods in Fluid Dynamics (Enschede, The Nethertlands), Springer-Verlag, Berlin, 1975, pp 247-253.