Van Zyl, Louwrens H2008-05-082008-05-081994-11Van Zyl, L.H. 1994. Integration of the supersonic kernel function. Journal of Aircraft, Vol. 31(6), pp. 1433-1435.0021-8669http://hdl.handle.net/10204/2245The article discusses ways in which the integrals resulting from a zero-order discontinuous pressure distribution can be arranged in such a way that they can be solved by either normal quadrature or curve fitting followed by analytical integration is shown. This ability amplifies the panel method for unsteady supersonic flow and is essential to model the discontinuities that occur in reality, e.g., at the supersonic leading or trailing edges and control surface hinge lines.enSupersonic kernal functionIntegrationZero-order discontinous pressure distributionAnalytical integrationSupersonic flowControl surface hinge linesIntegration of the supersonic kernel functionArticleVan Zyl, L. H. (1994). Integration of the supersonic kernel function. http://hdl.handle.net/10204/2245Van Zyl, Louwrens H "Integration of the supersonic kernel function." (1994) http://hdl.handle.net/10204/2245Van Zyl LH. Integration of the supersonic kernel function. 1994; http://hdl.handle.net/10204/2245.TY - Article AU - Van Zyl, Louwrens H AB - The article discusses ways in which the integrals resulting from a zero-order discontinuous pressure distribution can be arranged in such a way that they can be solved by either normal quadrature or curve fitting followed by analytical integration is shown. This ability amplifies the panel method for unsteady supersonic flow and is essential to model the discontinuities that occur in reality, e.g., at the supersonic leading or trailing edges and control surface hinge lines. DA - 1994-11 DB - ResearchSpace DP - CSIR KW - Supersonic kernal function KW - Integration KW - Zero-order discontinous pressure distribution KW - Analytical integration KW - Supersonic flow KW - Control surface hinge lines LK - https://researchspace.csir.co.za PY - 1994 SM - 0021-8669 T1 - Integration of the supersonic kernel function TI - Integration of the supersonic kernel function UR - http://hdl.handle.net/10204/2245 ER -