NASA_Software_Catalog_2014.pdf#sthash.Rk7M8wlL

GRAPE.107LEW-16851-1GRAPE is a two-dimensional elliptic grid generation code to be used with isolated airfoils. This modifiedversion of the software (with application for turbomachinery blades) can generate grids for the RVCQ3Dturbo-machinery analysis code.U.S. Release OnlyHigh-Speed Data ViewerMFS-31700-1The High-Speed Data Viewer computer software was developed for viewing high-frequency data recordedin the East and West Test Areas at Marshall Space Flight Center (MSFC).U.S. Release OnlyIceVal DatAssistantLEW-18343This NASA-developed technology provides an improved mechanism for managing the large volume of datagenerated and utilized in performing icing research.U.S. Release OnlyIntegrated Structural Analysis and Test ProgramGSC-14775-1This technology offers an innovative way of integrating analysis/test data to facilitate the mechanical verificationof space systems. The technology automates repetitive processes, provides faster pre-test analysis andtest reporting, facilitates test planning, and improves test execution.U.S. Government Purpose ReleaseInternational Space Station (ISS) Systems Integration Laboratory (ISIL)MSC-24341-1This NASA-developed software provides an open-source framework that consolidates ISS laboratory testfunctions. The technology automates the start-up process of the large ISIL test rig (including configurationvalidation) and provides test engineers with Web access to recorded test data for post-test analysis.U.S. Government Purpose ReleaseJet Noise Prediction Code (JeNo)LEW-18199JeNo is a Fortran 90 computer code that calculates the far-field sound spectral density produced by axisymmetricjets at user-specified observer locations and frequency ranges. The user must provide a structuredcomputational grid and also input a mean flow solution from a Reynolds-Averaged Navier Stokes (RANS).U.S. Release OnlyJet Noise Prediction Code (JeNo 2.5D)LEW-18199JeNo is a Fortran 90 computer code that evaluates the far-field turbulence-generated noise in non-axisymmetricjets. The propagation Green’s function is calculated along a user-specified azimuthal angle (line ofsight), but source volume integration is carried out in 3D. The user must provide a structured computationalgrid in a polar coordinate system and also input a mean flow solution from a Reynolds-Averaged NavierStokes (RANS).U.S. Release OnlyLag Model—A Turbulence Model for Attached and Separated FlowsARC-14645-1This NASA-developed technology includes a set of partial differential equations that augment the ReynoldsaveragedNavier-Stokes equation. By providing a mechanism that allows flow history to affect turbulencestresses, Lag Model mimics underlying physical processes to provide an improved turbulence model forflows with separation.U.S. Government Purpose Release4. System TestingNASA Technology Transfer Program Software Catalog 2014 33