Expanded FORTRAN 4 program for elastic scattering analyses
Expanded FORTRAN 4 program for elastic scattering analyses
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Expanded FORTRAN 4 program for elastic scattering analyses
FORTRAN programs for calculating lower ionosphere electron densities and collision frequencies
Comprehensive programming course begins with numerical systems and basic concepts, proceeds systematically through FORTRAN language elements, and concludes with discussion of programming techniques. Course is suitable either for individual study or for group study on informal basis.
FORTRAN program for computing coordinates of circular arc single and tandem turbomachinery blade sections on plane
FORTRAN program for calculating aerodynamic forces from pressure or velocity distributions on blade sections
Design of FORTRAN parallel task recognizer program
TREETRAN subroutine package in FORTRAN 4 for manipulation of tree structured data
FORTRAN 4 subroutines for coupling coefficients and matrix elements in quantum mechanical theory of angular momentum
FORTRAN program for computation of group tables, alphanumeric display
Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms
FORTRAN computer program for generating geometrical data of heat transfer code
Set of FORTRAN 4 subroutines to calculate mass flow rate of natural gas through nozzles, also thermodynamic functions such as compressibility factor, entropy, enthalpy, and specific heat
Quasi-three dimensional surface velocities and choking flow for turbomachine blade rows calculated by FORTRAN program
Numerical method and FORTRAN program for solving Poisson's equation over axisymmetric regions of spherical body
FORTRAN 4 program /FITLOS/ for fitting low-order polynomial splines of two and three degrees by least squares method
Synthesis of structural dynamic systems using digital computer and FORMA(FORTRAN Matrix Analysis)
FORTRAN 5 digital computer program for predicting dynamic response of Apollo command module to earth impact
Coordinates for circular arc blade section of aircraft high speed compressor gas turbines were computed using FORTRAN 4 program. Aerodynamic configurations studied include single segment airfoils, airfoils with slots, and mutiple segment tandem arranged airfoil.