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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
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
 Vivek Ahuja
 (334) 332-6078
Business Contact
 Roy Hartfield
Phone: (334) 444-8523
Research Institution
 Utah State University
 Douglas Hunsaker
4000 Old Main Hill
Logan, UT 84322-4000
United States

 (435) 797-8404
 Nonprofit College or University

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. *

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