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ResearchSouth, Inc.

Details

Name: ResearchSouth, Inc.
Jurisdiction: Alabama
Legal type: Domestic Corporation
Status: Dissolved
Date of registration: 24 Mar 1993 (32 years ago)
Date of dissolution: 31 Jan 2017
Entity Number: 000-155-707
Register Number: 000155707
ZIP code: 35816
County: Madison
Place of Formation: Madison County
Registered Office Street Address: 555 SPARKMAN DRIVE STE 818HUNTSVILLE, AL 35816
Authorized Capital: $100

Activities SELLING ENGINEERING MECHANICS & OTHER SOFTWARE

Commercial and government entity program

CAGE number Status Type Established CAGE Update Date CAGE Expiration SAM Expiration
02SH4 Active Non-Manufacturer 1995-03-24 2014-05-30 No data No data

Contact Information

POC BETTY C. BETTY C. SPRADLEY
Phone +1 256-721-1769
Fax +1 256-430-3278
Address 555 SPARKMAN DR NW 1612, HUNTSVILLE, AL, 35816 3431, UNITED STATES

Ownership of Offeror Information

Highest Level Owner Information not Available
Immediate Level Owner Information not Available
List of Offerors (0) Information not Available

Incorporator

Name Role
SPRADLEY, BETTY C Incorporator
SPRADLEY, LAWRENCE W Incorporator

Agent

Name Role
SPRADLEY, LAWRENCE W Agent

Awards

Contract Type Award or IDV Flag PIID Start Date Current End Date Potential End Date
DCA AWARD NNX11CC70C 2011-08-15 2013-07-28 2013-07-28
Unique Award Key CONT_AWD_NNX11CC70C_8000_-NONE-_-NONE-
Awarding Agency National Aeronautics and Space Administration
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Description

Title THE INNOVATION OF OUR PHASE II STTR PROGRAM IS TO DEVELOP AND PROVIDE TO NASA AUTOMATIC MESH GENERATION SOFTWARE FOR THE SIMULATION OF FLUID FLOWS USING REYNOLDS-AVERAGED NAVIER-STOKES CODES. AS A RESULT OF THE SUCCESSFUL PHASE I WORK, THESE NEW TOOLS ARE NOW CAPABLE OF GENERATING HIGH-QUALITY, HIGHLY-STRETCHED (ANISOTROPIC) MESHES IN BOUNDARY LAYER REGIONS AND TRANSITION SMOOTHLY TO INVISCID FLOW REGIONS, EVEN IN AN ADAPTIVE CONTEXT. THE SIGNIFICANCE IS THAT OUR METHOD HAS THE ABILITY TO GENERATE A BOUNDARY LAYER MESH WHILE KEEPING INTACT THE PREVIOUS ADAPTATION PROCEDURES FROM NON VISCOUS SIMULATIONS. THIS LEADS TO A NATURAL COUPLING BETWEEN BOUNDARY LAYER MESH GENERATION AND ANISOTROPIC MESH ADAPTATION. ALL OF THE PHASE I OBJECTIVES WERE MET AND ALL TASKS WERE COMPLETED SUCCESSFULLY. THE PHASE II PROJECT WILL INCLUDE IMPROVEMENTS IN SURFACE REMESHING, CODING FOR OPTIMAL SPEED AND INCREASED ROBUSTNESS OF THE SOLVERS, ADDING A MESH OPTIMIZATION MODULE, PROVIDING A LINK TO GENERAL CAD PACKAGES, INCLUDE UNSTEADY COUPLING WHERE THE BOUNDARY LAYER MESH REFINEMENT EVOLVES IN TIME, CONDUCT FURTHER VALIDATION AND VERIFICATION ON NASA MODELS BY RUNNING FLOW CASES WITH OUR SOLVER, DOCUMENTING THE PROJECT, AND DELIVERING THE NEW MESHING SOFTWARE TO NASA.
NAICS Code 541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product and Service Codes AR11: R&D-AERO & SPACE TECH-B RES

Recipient Details

Recipient RESEARCHSOUTH INC
UEI N3RYGJYNSEJ5
Legacy DUNS 928516442
Recipient Address UNITED STATES, 555 SPARKMAN DR NW # 1612, HUNTSVILLE, 358163431
PO AWARD NNX10CF75P 2010-09-01 2011-01-28 2011-01-28
Unique Award Key CONT_AWD_NNX10CF75P_8000_-NONE-_-NONE-
Awarding Agency National Aeronautics and Space Administration
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Description

Title THIS PROPOSAL OFFERS TO PROVIDE NASA WITH AN AUTOMATIC MESH GENERATOR FOR THE SIMULATION OF AERODYNAMIC FLOWS USING REYNOLDS-AVERAGES NAVIER-STOKES (RANS) MODELS. THE TOOLS WILL BE CAPABLE OF GENERATING HIGH-QUALITY, HIGHLY-STRETCHED (ANISOTROPIC) GRIDS IN BOUNDARY LAYER REGIONS AND TRANSITION SMOOTHLY TO INVISCID FLOW REGIONS EVEN IN AN ADAPTIVE CONTEXT. THE OBJECTIVE OF THE WORK IS TO OFFER A UNIFIED VIEW FOR GENERATING QUALITY AND ROBUST RANS MESHES COUPLED NATURALLY WITH ANISOTROPIC MESH ADAPTATION. OUR INNOVATION IS TO VIEW THE ANISOTROPIC MESH GENERATION WITHIN THE RIEMANNIAN METRIC FRAMEWORK WHICH THUS FAR HAS BEEN USED EXCLUSIVELY IN ANISOTROPIC MESH ADAPTATION. USING THE METRIC-BASED FRAMEWORK ALLOWS MUCH EASIER HANDLING OF THE LARGE MESH SIZE RATIOS INVOLVED IN THE COMPUTATION, WHEREAS TRADITIONAL METHODS USE THE EUCLIDEAN FRAMEWORK TO COMPUTE DISTANCE AND VOLUME. THIS INNOVATIVE VIEW TO GENERATE THESE MESHES MAKES THE ENTIRE PROCEDURE MORE GENERIC AND MUCH MORE ROBUST. THE EMPHASIS IS BEING PUT ON DERIVING A COMPLETELY AUTOMATIC PROCESS TO GENERATE QUALITY AND ROBUST ANISOTROPIC MESHES. OUR EXISTING AND PROVEN SOFTWARE PACKAGE WILL BE MODIFIED TO INCLUDE THESE INNOVATIVE METHODS. A NASA TEST CASE WILL BE COMPUTED FOR VALIDATION OF THE METHODS. THE SOFTWARE WILL BE DELIVERED IN PHASE II.
NAICS Code 541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product and Service Codes AR11: R&D-AERO & SPACE TECH-B RES

Recipient Details

Recipient RESEARCHSOUTH INC
UEI N3RYGJYNSEJ5
Legacy DUNS 928516442
Recipient Address UNITED STATES, 555 SPARKMAN DR NW # 1612, HUNTSVILLE, 358163431
DCA AWARD NNL08AA33C 2008-04-03 2011-04-02 2011-04-02
Unique Award Key CONT_AWD_NNL08AA33C_8000_-NONE-_-NONE-
Awarding Agency National Aeronautics and Space Administration
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Description

Title HYPERSONICS #0017, NRA #NNH07ZEA001N, VEHICLE TECHNOLOGY INTEGRATION, MULTIDISCIPLINARY MODELING SOFTWARE FOR ANALYSIS, DESIGN, AND OPTIMIZATION OF HRRLS VEHICLES.
NAICS Code 541511: CUSTOM COMPUTER PROGRAMMING SERVICES
Product and Service Codes AR24: R&D-SPACE SCIENCE & APPL-ENG DEV

Recipient Details

Recipient RESEARCHSOUTH INC
UEI N3RYGJYNSEJ5
Legacy DUNS 928516442
Recipient Address UNITED STATES, 555 SPARKMAN DR NW # 1612, HUNTSVILLE, 358163431

Date of last update: 01 Aug 2024

Sources: Alabama Secretary of State