The method is capable of generating approximations of arbitrary accuracy. It is based on approximating the algebraic part of the nonelementary integrals in the kernel by exponential functions and then integrating termwise. The exponent spacing in the approximation is a geometric sequence. The coefficients and exponent multiplier of the exponential approximation are computed by least squares so the method is completely automated. Exponential approximates generated in this manner are two orders of magnitude more accurate than the exponential approximation that is currently most often used for this purpose. The method can be used to generate approximations to attain any desired trade-off between accuracy and computing cost
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
Progress in the development of computational methods for steady and unsteady aerodynamics has perenn...
Two transonic computational schemes which are based on the Integral Equation Formulation of the full...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
Integral equation relating general time-dependent lift & downwash distributions of finite wings in s...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
The derivation of the integral equation which involves this kernel function, originally performed el...
Finite difference methods for unsteady transonic flow frequency use simplified equations in which ce...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
A function integral equation governing the unsteady motion of a supersonic cascade is derived. Vario...
ABSTRACT: Prediction of unsteady aerodynamic loads is still the most challenging task in flutter aer...
An integral equation method for solving the full potential equation has been developed for three dim...
A development was the time linearization of the density function. This linearization reduces the sol...
The method of integral relations is applied in a one-strip approximation to the perturbation equatio...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
Progress in the development of computational methods for steady and unsteady aerodynamics has perenn...
Two transonic computational schemes which are based on the Integral Equation Formulation of the full...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
Integral equation relating general time-dependent lift & downwash distributions of finite wings in s...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
The derivation of the integral equation which involves this kernel function, originally performed el...
Finite difference methods for unsteady transonic flow frequency use simplified equations in which ce...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
A function integral equation governing the unsteady motion of a supersonic cascade is derived. Vario...
ABSTRACT: Prediction of unsteady aerodynamic loads is still the most challenging task in flutter aer...
An integral equation method for solving the full potential equation has been developed for three dim...
A development was the time linearization of the density function. This linearization reduces the sol...
The method of integral relations is applied in a one-strip approximation to the perturbation equatio...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
Progress in the development of computational methods for steady and unsteady aerodynamics has perenn...
Two transonic computational schemes which are based on the Integral Equation Formulation of the full...