A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow. Part 1. Description and application

A detailed description is given of the theory underlying a panel method (NLRAERO) for the computation of the velocity and pressure distribution, load distributions, forces and moments on complex configurations in linearized subsonic or supersonic flow. The method can be considered as an improved and extended version of Woodward's method USSAERO....

A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow. Part 2. Evaluation of aerodynamic influence coefficients

A panel method for the computation of the velocity and pressure distribution on complex configurations in subsonic or supersonic flow has been described in Part I of the present report. This part of the report describes the evaluation of the aerodynamic influence coefficients. Expressions are derived for the (near-field) influence coefficients...

A computational model for the calculation of the flow about wings with loading-edge vortices