Add to ORKGDetails are given of a numerical solution of the integral equation which relates oscillatory or steady lift and downwash distributions in subsonic flow. The procedure has been programmed for the IBM 704 electronic data processing machine and yields the pressure distribution and some of its integrated properties for a given Mach number and frequency and for several modes of oscillation in from 3 to 4 minutes, results of several applications are presented
A general method for steady and oscillatbry, subsonic and supersonic, poten-tial linearized aerodyna...
A computer program has been developed to account approximately for the effects of finite wing thickn...
Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls b...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
A method is presented for calculating the loading on a finite wing oscillating in subsonic or sonic ...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
The derivation of the integral equation which involves this kernel function, originally performed el...
A description of and user's manual are presented for one of a group of FORTRAN programs which, toget...
The application of a kernel function lifting surface method to three dimensional, thin wing theory i...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
The SOUSSA (steady, oscillatory, and unsteady subsonic and supersonic aerodynamics) program is the c...
Integral equation relating general time-dependent lift & downwash distributions of finite wings in s...
Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...
A digital computer program has been developed to calculate unsteady loadings caused by motions of li...
A general method for steady and oscillatbry, subsonic and supersonic, poten-tial linearized aerodyna...
A computer program has been developed to account approximately for the effects of finite wing thickn...
Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls b...
This report treats the Kernel function of the integral equation that relates a known or prescribed d...
The theory, results and user instructions for an aerodynamic computer program are presented. The the...
A method is presented for calculating the loading on a finite wing oscillating in subsonic or sonic ...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
The derivation of the integral equation which involves this kernel function, originally performed el...
A description of and user's manual are presented for one of a group of FORTRAN programs which, toget...
The application of a kernel function lifting surface method to three dimensional, thin wing theory i...
This report treats the Kernel function of an integral equation that relates a known prescribed downw...
The SOUSSA (steady, oscillatory, and unsteady subsonic and supersonic aerodynamics) program is the c...
Integral equation relating general time-dependent lift & downwash distributions of finite wings in s...
Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...
A digital computer program has been developed to calculate unsteady loadings caused by motions of li...
A general method for steady and oscillatbry, subsonic and supersonic, poten-tial linearized aerodyna...
A computer program has been developed to account approximately for the effects of finite wing thickn...
Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls b...