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A Multi-Fidelity Supersonic Flow Solver for Preliminary Design & Optimization
Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA864922P0081
Agency Tracking Number: FX21B-TCSO1-0228
Amount:
$50,000.00
Phase:
Phase I
Program:
STTR
Solicitation Topic Code:
AF21B-TCSO1
Solicitation Number:
X21.B
Timeline
Solicitation Year:
2021
Award Year:
2022
Award Start Date (Proposal Award Date):
2021-11-03
Award End Date (Contract End Date):
2022-02-03
Small Business Information
1919 North Ashe Ct.
Auburn, AL
36830-1111
United States
DUNS:
078301615
HUBZone Owned:
No
Woman Owned:
No
Socially and Economically Disadvantaged:
No
Principal Investigator
Name: Vivek Ahuja
Phone: (334) 332-6078
Email: vivek.ahuja@researchinflight.com
Phone: (334) 332-6078
Email: vivek.ahuja@researchinflight.com
Business Contact
Name: Roy Hartfield
Phone: (334) 444-8523
Email: roy.hartfield@researchinflight.com
Phone: (334) 444-8523
Email: roy.hartfield@researchinflight.com
Research Institution
Name: Utah State University
Contact: Douglas Hunsaker
Address:
Phone: (435) 797-8404
Type: Nonprofit College or University
Contact: Douglas Hunsaker
Address:
4000 Old Main Hill
Logan, UT
84322-4000
United States
Phone: (435) 797-8404
Type: Nonprofit College or University
Abstract
Research in Flight (RIF) and Utah State University (USU) are proposing the development of a novel supersonic panel method solver which runs on an unstructured mesh and uses low-order surface-vorticity distributions. The solver will resolve linearized supe
* Information listed above is at the time of submission. *
