Users manual: MSFC crack growth analysis computer program
The input and output formats and options are described along with the technical approaches used within the computer program. Included are example data and problems.
Creager, M.↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Development of a computer program to obtain ordinates for NACA 4-digit, 4-digit modified, 5-digit, and 16 series airfoils
A computer program developed to calculate the ordinates and surface slopes of any thickness, symmetrical or cambered NACA airfoil of the 4-digit, 4-digit modified, 5-digit, and 16-series airfoil families is presented. The program produces plots of the airfoil nondimensional ordinates and a punch card output of ordinates in the input format of a readily available program for determining the pressure distributions of arbitrary airfoils in subsonic potential viscous flow.
Ladson, C. L.↗
A computer program for the use of sensitivity analysis in display evaluation
A description is provided of the Display Evaluation computer program, some results of this program and comparison of these results with a simple experiment. A detailed description of the experiment and data analysis are also included.
Mout, M. L.↗
VIBRA: An interactive computer program for steady-state vibration response analysis of linear damped structures
An interactive steady state frequency response computer program with graphics is documented. Single or multiple forces may be applied to the structure using a modal superposition approach to calculate response. The method can be reapplied to linear, proportionally damped structures in which the damping may be viscous or structural. The theoretical approach and program organization are described. Example problems, user instructions, and a sample interactive session are given to demonstate the program's capability in solving a variety of problems.
Bowman, L. M.↗
Manual of phosphoric acid fuel cell stack three-dimensional model and computer program
A detailed distributed mathematical model of phosphoric acid fuel cell stack have been developed, with the FORTRAN computer program, for analyzing the temperature distribution in the stack and the associated current density distribution on the cell plates. Energy, mass, and electrochemical analyses in the stack were combined to develop the model. Several reasonable assumptions were made to solve this mathematical model by means of the finite differences numerical method.
Lu, C. Y.↗
Computer program for calculation of complex chemical equilibrium compositions and applications. Supplement 1: Transport properties
An addition to the computer program of NASA SP-273 is given that permits transport property calculations for the gaseous phase. Approximate mixture formulas are used to obtain viscosity and frozen thermal conductivity. Reaction thermal conductivity is obtained by the same method as in NASA TN D-7056. Transport properties for 154 gaseous species were selected for use with the program.
Gordon, S.↗
Basis And Application Of The CARES/LIFE Computer Program
Report discusses physical and mathematical basis of Ceramics Analysis and Reliability Evaluation of Structures LIFE prediction (CARES/LIFE) computer program, described in "Program for Evaluation of Reliability of Ceramic Parts" (LEW-16018).
Nemeth, Noel N.↗
Computer program for generating kinematic earthquake rupture models using Irikura and Miyake's method.
GEN_SRF_4 is a computer program for generation kinematic earthquake rupture models for use in ground motion modeling and simulations of earthquakes. The output is an ascii SRF formatted file containing kinematic rupture parameters.
Pitarka, Arben↗
BUCLAP2: A computer program for instability analysis of laminated long plates subjected to combined inplane loads
This program description document describes the program structure and the design details of a CDC 6600 FORTRAN 4 digital computer program, BUCLAP2, which uses minimum energy principles to do an elastic stability analysis of curved and flat laminated rectangular long plates subjected to combined inplane normal and shear loads. Given the geometry, the material properties, and slected boundary conditions for the plate element, the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the program calculates the minimum buckling load for various wave lengths. The two parallel ends of the long plate must be simply supported and arbitrary elastic boundary conditions may be imposed along either one or both external longitudinal sides. For guide to program use, see
Halstead, D. W.↗
Fortran ii computer program for the evaluation of a donnell type of differential equation for an orthotropic circular conical shell
Fortran ii computer program for evaluation of donnell type differential equation for orthotropic circular-conical shell
DONNELL EQUATION↗
A computer program for a line by line calculation of spectra from diatomic molecules and atoms assuming a Voigt line profile
Computer program for line-by-line calculation of spectra from diatomic molecules and atoms assuming Voigt line profile
Arnold, J. O.↗
FEDGE - A general-purpose computer program for Finite Element Data Generation. Volume 1 - User's manual
Users manual for /FEDGE/ Finite Element Data Generation computer program - Vol. 1
Akyuz, F. A.↗
A computer program to determine equilibrium- air flow-field data about a blunt body by the method of integral relations
Computer program for determination of equilibrium air flow field data about blunt bodies by integral relations method
Taylor, F. W.↗
Computer program for design of two-dimensional sharp-edged-throat supersonic nozzle with boundary layer correction
FORTRAN 4 computer program for design of sharp-edged-throat supersonic nozzles with boundary layer correction
Goldman, L. J.↗
A computer program for calculating inviscid, adiabatic flow about blunt bodies traveling at supersonic and hypersonic speeds at angle of attack
Computer program for determining inviscid flow around blunt bodies at supersonic and hypersonic speeds - users manual
Barnwell, R. W.↗
Computer program for design of two-dimensional supersonic turbine rotor blades with boundary-layer correction
A FORTRAN 4 computer program for the design of two-dimensional supersonic rotor blade sections corrected for boundary-layer displacement thickness is presented. The ideal rotor is designed by the method of characteristics to produce vortex flow within the blade passage. The boundary-layer parameters are calculated by Cohen and Reshotoko's method for laminar flow and Sasman and Cresci's method for turbulent flow. The program input consists essentially of the blade surface Mach number distribution and total flow conditions. The primary output is the corrected blade profile and the boundary-layer parameters.
Goldman, L. J.↗
Computer program for quasi-one-dimensional compressible flow with area change and friction - Application to gas film seals
A computer program is presented for compressible fluid flow with friction and area change. The program carries out a quasi-one-dimensional flow analysis which is valid for laminar and turbulent flows under both subsonic and choked flow conditions. The program was written to be applied to gas film seals. The area-change analysis should prove useful for choked flow conditions with small mean thickness, as well as for face seals where radial area change is significant. The program is written in FORTRAN 4.
Zuk, J.↗
Computer program for calculation of real gas turbulent boundary layers with variable edge entropy
A user's manual for a computer program which calculates real gas turbulent boundary layers with variable edge entropy on a blunt cone or flat plate at zero angle of attack is presented. An integral method is used. The method includes the effect of real gas in thermodynamic equilibrium and variable edge entropy. A modified Crocco enthalpy velocity relationship is used for the enthalpy profiles and an empirical correlation of the N-power law profile is used for the velocity profile. The skin-friction-coefficient expressions of Spalding and Chi and Van Driest are used in the solution of the momentum equation and in the heat-transfer predictions that use several modified forms of Reynolds analogy.
Boney, L. R.↗