This document is the programmer's guide for the GNAT computer program developed under MSC/TRW Task 705-2, Apollo cryogenic storage system analysis, subtask 2, is reported. Detailed logic flow charts and compiled program listings are provided for all program elements
The NATA code is a computer program for calculating quasi-one-dimensional gas flow in axisymmetric n...
The operational steps, data descriptions, and program code for the new NASTRAN hydroelastic analysis...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
An appendix to the programmers manual for the mathematical model pertaining to the design of cryogen...
Digital computer program for geometrically nonlinear analysis of thin shells of revolution under axi...
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
A number of computer codes are available for performing thermal analysis of solid rocket motor nozzl...
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
Computer programs for analysis of liquid heat exchangers for convective and radiative systems of duc...
The Lewis Research Center's cryogenic fluid management program flight concept definition is presente...
This program was designed to be an editor for the Lewis Chemical Equilibrium program input files and...
Modified P function applied to turbulent mixing of three coaxial, axisymmetric jets of reactive gase
Computer programs for simulation of reconfigurable guidance and control system operation - Vol.
A FORTRAN IV program for analyzing the nozzle flow for a hypersonic scramjet by a two dimensional se...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
The NATA code is a computer program for calculating quasi-one-dimensional gas flow in axisymmetric n...
The operational steps, data descriptions, and program code for the new NASTRAN hydroelastic analysis...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
An appendix to the programmers manual for the mathematical model pertaining to the design of cryogen...
Digital computer program for geometrically nonlinear analysis of thin shells of revolution under axi...
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
A number of computer codes are available for performing thermal analysis of solid rocket motor nozzl...
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
Computer programs for analysis of liquid heat exchangers for convective and radiative systems of duc...
The Lewis Research Center's cryogenic fluid management program flight concept definition is presente...
This program was designed to be an editor for the Lewis Chemical Equilibrium program input files and...
Modified P function applied to turbulent mixing of three coaxial, axisymmetric jets of reactive gase
Computer programs for simulation of reconfigurable guidance and control system operation - Vol.
A FORTRAN IV program for analyzing the nozzle flow for a hypersonic scramjet by a two dimensional se...
The computer program written in support of the problem to determine aerodynamic influence coefficien...
The NATA code is a computer program for calculating quasi-one-dimensional gas flow in axisymmetric n...
The operational steps, data descriptions, and program code for the new NASTRAN hydroelastic analysis...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...