SBIR/STTR Research Award

Automated, Fast CFD Solver Technologies for Hypersonics

Award identifier 5f7fb9aacddfa9afcdd5be51a6898de192aaed8b31d105aa528d0fd95dba8f14Awarding agency Department of Defense · Navy

Award amount

$139,855

Program and phase

SBIR · Phase I

Award year

2025

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
GOHYPERSONIC INCORPORATED
Proposal award date
2025-07-07
Contract end date
2026-01-07
UEI
E2DLZMNA2361
Solicitation number
25.1
Topic code
N251-060

Research abstract

This proposal seeks to produce an approachable, ìsingle click-to-solutionî, software tool capable of producing high quality laminar solutions of hypersonic wall-bounded flows. Laminar to turbulence boundary layer transition poses a difficult challenge in hypersonic vehicle design. Large uncertainties drive design requirements to be overly cautious in thermal protection systems and control design due to assumed heating and drag augmentation imposed by the presence of a turbulence boundary layer.ÝAdvances in stability analysis provide increased accuracy on transition location over heritage methods, but require high-fidelity simulated base flows to operate on. High-fidelity simulations of hypersonic flows currently require access to high-performance computers, robust numerics, complicated solver interfaces/operation, involved pre- and post-processing analysis, artisan level mesh generation skills, and more. These factors present a large barrier to entry to those who are familiar with the physics of high-enthalpy environments.ÝGHI proposes a simplified software tool capable of producing laminar solutions on modern CPU/GPU workstations. The solutions will be high-fidelity and used to perform more modern stability analysis to predict transition locations more accurate as compared to heritage correlations. GHI will leverage current and past efforts in software development and hypersonic simulations to package an approachable tool capable of generating laminar flows accurate enough to perform stability analysis on. The tool will automatically generate meshes, identify critical flow features and re-generate or refine the computational mesh, removing the requirement of mesh generation and speeding up time to solution. The multi-step mesh generation process will ultimately yield accurate laminar flowfields.Ý The end product will be a single interface that non-advanced users can interact with on a modern CPU/GPU desktop PC and generate solutions with a 10x speed up over current state-of-the-art solvers. The solutions will be available in data formats consistent with current stability analysis tools.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

28 SBIR/STTR records share this UEI (2006–2026). Reported award amounts total $12,672,767. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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