SBIR/STTR Research Award

A Fast and Robust PIMPLE-Based Algebraic VOF Method for Two-Phase Compressible Flows

Award identifier 43cea6a789f11867c0707016270d61190f2e01fb485e4059384ed6670cc393a4Awarding agency National Aeronautics and Space Administration

Award amount

$124,923

Program and phase

SBIR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
STREAMLINE NUMERICS, INC.
Proposal award date
2020-08-03
Contract end date
2021-03-01
UEI
YSLNMSL67YC7
Solicitation number
SBIR_20_P1
Topic code
H10

Research abstract

This project is geared towards a computationally efficient, robust computational fluid dynamics (CFD) tool for simulating unsteady multiphase flows of critical importance to NASA in their ground and launch systems processing technologies.nbsp; The key features of the proposed work are: (a) Significant cost reduction in unsteady simulations via the PIMPLE algorithm, and (b) a fast and robust Algebraic Volume of Fluid (AVOF) method for two-phase flows. This methodology will be developed in the Loci-STREAM CFD code and will allow significantly reduced solution time for unsteady simulations of cavitating flows and fluid-structure interaction (FSI) simulations at NASA, as well as simulation of liquid jets and sprays such as in NASA/SSCrsquo;s B-2 test facility. The work will involve: (a) upgrading the unsteady methodology in Loci-STREAM by implementing the PIMPLE algorithm, and will improve runtime of cavitation and FSI simulations by a factor of 3ndash;5, and (b) Implementing an algebraic VOF method using compressive schemes which will allow simulations of two-phase flows (involving liquid jets) in a robust and more efficient manner (significantly faster solution times) manner than is currently possible with the geometric VOF available in Loci-STREAM. Two types of compressive schemes will be implemented: (a) Schemes based on the Normalized Variable Diagram (NVD) and Convection Boundedness Criterion (CBC), and (b) Flux-limiting schemes with the total variation diminishing (TVD) condition. The following application areas will benefit immediately from this project: (i) Unsteady cavitation in cryogenic propellant tanks, valve flows, and run lines, (ii) Transient fluid structure interaction (FSI) between cryogenic fluids and immersed components to predict the dynamic loads, frequency response of facilities, and (c) Modeling of liquid (water) jets including their breakup for flow tests on the B-2 test stand to verify the water system capability and functionality in support of the SLS.

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

32 SBIR/STTR records share this UEI (2004–2022). Reported award amounts total $11,051,944. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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