Documented is an aeronautical geometry conversion package which translates wave-drag geometry into the Langley Wireframe Geometry Standard (LaWGS) format and then into a format which is used by the Supersonic Implicit Marching Potential (SIMP) program. The programs described were developed by Computer Sciences Corporation for the Advanced Vehicles Division/Advanced Concepts Branch at NASA Langley Research Center. Included also are the input and output from a benchmark test case
Test program for cap section mesh fabrication in prototype space erectable satellite developmen
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
Algorithms were developed for the extraction of two components of mean velocity, standard deviation,...
A star simulator is described which is capable of simulating a field of three or more stars in respo...
The delineation of areas subject to inundation by means of remotely-sensed data acquisition represen...
A computer code HALIS, designed to compute the three dimensional flow about shuttle like configurati...
Photoviscoelastic method for stress analysis of two dimensional viscoelastic model
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
This report describes the results of a small study program in support of the design studies for NASA...
Transmission loss from precipitation scatter interference between space and earth communication syst...
This report describes computer program NOYFB, a method of determining the static configuration of s...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
An explicit-implicit and an implicit two-dimensional Navier-Stokes code along with various grid gene...
Profile-drag coefficients published from tests in the N.A.C.A. variable-density tunnel (Technical Re...
Submitted in partial fulfillment of the requirements of the degree of Master of Science at the Mas...
Test program for cap section mesh fabrication in prototype space erectable satellite developmen
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
Algorithms were developed for the extraction of two components of mean velocity, standard deviation,...
A star simulator is described which is capable of simulating a field of three or more stars in respo...
The delineation of areas subject to inundation by means of remotely-sensed data acquisition represen...
A computer code HALIS, designed to compute the three dimensional flow about shuttle like configurati...
Photoviscoelastic method for stress analysis of two dimensional viscoelastic model
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
This report describes the results of a small study program in support of the design studies for NASA...
Transmission loss from precipitation scatter interference between space and earth communication syst...
This report describes computer program NOYFB, a method of determining the static configuration of s...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
An explicit-implicit and an implicit two-dimensional Navier-Stokes code along with various grid gene...
Profile-drag coefficients published from tests in the N.A.C.A. variable-density tunnel (Technical Re...
Submitted in partial fulfillment of the requirements of the degree of Master of Science at the Mas...
Test program for cap section mesh fabrication in prototype space erectable satellite developmen
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
Algorithms were developed for the extraction of two components of mean velocity, standard deviation,...