Menu

 

The NASA Task Book
Advanced Search     

Project Title:  High-Fidelity Experiments and Computations of Transient Two-Phase Flow for Understanding Cryogenic Propellant Tank Transfer Reduce
Images: icon  Fiscal Year: FY 2024 
Division: Physical Sciences 
Research Discipline/Element:
Physical Sciences: FLUID PHYSICS--Fluid physics 
Start Date: 11/30/2021  
End Date: 11/29/2026  
Task Last Updated: 10/01/2023 
Download report in PDF pdf
Principal Investigator/Affiliation:   Miljkovic, Nenad  Ph.D. / University of Illinois, Urbana-Champaign 
Address:  Department of Mechanical Science and Engineering 
105 S Mathews Ave, 2136 Mechanical Engineering Laboratory 
Urbana , IL 61801-2924 
Email: nmiljkov@illinois.edu 
Phone: 617-981-9247  
Congressional District: 13 
Web:  
Organization Type: UNIVERSITY 
Organization Name: University of Illinois, Urbana-Champaign 
Joint Agency:  
Comments:  
Co-Investigator(s)
Affiliation: 
Yazdani, Miad  Ph.D. United Technologies Corporation 
Key Personnel Changes / Previous PI: None PI changes to report. A postdoctoral associate was hired to work on the project. He started his role on September 1 2023 and will continue work through 2024.
Project Information: Grant/Contract No. 80NSSC22K0294 
Responsible Center: NASA GRC 
Grant Monitor: Chao, David  
Center Contact: 216-433-8320 
david.f.chao@nasa.gov 
Unique ID: 14803 
Solicitation / Funding Source: 2020 Physical Sciences NNH20ZDA012N: Fluid Physics. Appendix A 
Grant/Contract No.: 80NSSC22K0294 
Project Type: FLIGHT,GROUND 
Flight Program: ISS 
No. of Post Docs:
No. of PhD Candidates:
No. of Master's Candidates:
No. of Bachelor's Candidates:
No. of PhD Degrees:
No. of Master's Degrees:
No. of Bachelor's Degrees:
Program--Element: FLUID PHYSICS--Fluid physics 
Flight Assignment/Project Notes: ISS

Task Description: Cryogenic chilldown governs initial stages of cryogen transport. Chilldown involves complicated hydrodynamic and thermal interactions between the liquid, vapor, and channel wall. Large initial temperature differences between the walls and the cryogen create rapid evaporation and large pressure and temperature fluctuation. Although work has attempted to identify transient flow boiling regimes, local surface temperatures, and heat fluxes, chilldown remains poorly understood due to the lack of experimental techniques capable of attaining high spatio-temporal resolution in both optical and infrared (IR) spectra. Furthermore, a lack of computational methods exists which can predict transient flow boiling and chilldown for a variety of length and time scales, and working fluid and system geometries.

Here, we propose a collaborative effort between the University of Illinois, Urbana-Champaign (UIUC) and Raytheon Technologies (RTX) to develop fundamental understanding of chilldown using complementary high-fidelity experiments and computations. Internal flow pattern variations ranging from the film, transition, nucleate, to convection flow boiling using FC-72 and liquid nitrogen (LN2) in NASA relevant aluminum and stainless steel tubes, will be studied. We will use in-liquid endoscopy to study in-situ quench front propagation during FC-72 and LN2 flow boiling. The synchronous use of internal optical and external IR visualization will enable the gaining of a rigorous understanding of the thermal-fluidic behavior occurring in the near-wall region during chilldown and transient flow boiling. The obtained parameters, such as the quench front propagation rate and the temperature and heat flux distributions near the quench front, will then be used to validate high-fidelity computations. The computational framework at RTX leverages the established foundation that is capable of predicting the thermal and hydrodynamic behavior of multiphase flows in convective boiling and condensation regimes. The multiple scales associated with chilldown and two-phase flow boiling will be addressed through a combination of the previously developed Direct Numerical Simulation (DNS) approach for the nucleation near the wall, the Large Eddy Simulation (LES) formulation for the macroscopic transport in the core, and a novel coupling scheme for transporting the information across these scales. While the inherent transient phenomena such as solid condition, nucleation, and regime transition are an integral part of this framework, the model will be modified to allow transient boundary and operating conditions due to the operation of the tank during chilldown. The simulation will provide highly resolved information on the thermal and flow characteristics of two-phase cryogenic flow during the chilldown process and particularly the transient evolution of the flow regime during boiling. The model predictions will continually be validated against the high-fidelity experimental measurements over a range of test conditions. The work is broken down into tasks, which are briefly defined by:

1) Experimental analysis of transient heat transfer and pressure fluctuation during chilldown in Earth gravity with FC-72; 2) Integration of synchronous optical and IR visualization of chilldown with FC-72 and LN2 in Earth gravity for a variety of conditions including tube material, tube size, pressure difference, initial system temperature, and cryogen flow rate; 3) Simulations of transient flow boiling and chilldown in Earth gravity with FC-72 in order to provide physical insight on how the flow regime and boiling regime evolve over the course of chilldown; and 4) FC-72 flow boiling tests in microgravity with simulation validation.

The outcomes of the on-Earth experiments will guide testing in microgravity on the Flow Boiling and Condensation Experiment (FBCE) on the International Space Station (ISS) to better understand the time-varying system pressure and temperatures during the cryogenic propellant transfer process.

Research Impact/Earth Benefits: Cryogenic chilldown governs initial stages of cryogen transport. Flow pattern variation and quench front propagation are crucial for analyzing and understanding the mechanism of chilldown.

Task Progress & Bibliography Information FY2024 
Task Progress: In the last reporting year, we completed the assembly of the loop for FC-72 but the assembled setup was just in its infancy and some issues happened when we got some preliminary results based on the verification tests. Therefore, in this early reporting year, we made several improvements to the setup to ensure the experiments and measurements operate at the desired conditions. The work on terrestrial experiments and microgravity experiments kept moving forward. We conducted terrestrial chilldown experiments with FC-72 in both copper and stainless-steel tube sections in the low Reynolds number region (<=10,000) and obtained useful heat transfer and pressure information for each test condition. The data helped us understand how the mass flow rates, subcooling, and thermal properties of the test section materials affect the transient flow boiling during the chilldown process.

In addition, as we confirmed the collaboration with Case Western Reserve University (CWRU) on the science requirement documents (SRD) in May of last year, we continuously promoted the progress of integrating our SRD and completed the integrated science requirements documents (ISRD) in September of this year after several rounds of discussion with NASA engineers and CWRU; some associated documents, e.g., the Experiment Data and Management Plan (EDMP) and Mission Requirements Documents, have also been prepared for the Science Requirements Review (SRR), which is due to occur in January of next year (2024).

Bibliography: Description: (Last Updated: 09/29/2022) 

Show Cumulative Bibliography
 
 None in FY 2024
Project Title:  High-Fidelity Experiments and Computations of Transient Two-Phase Flow for Understanding Cryogenic Propellant Tank Transfer Reduce
Images: icon  Fiscal Year: FY 2023 
Division: Physical Sciences 
Research Discipline/Element:
Physical Sciences: FLUID PHYSICS--Fluid physics 
Start Date: 11/30/2021  
End Date: 11/29/2026  
Task Last Updated: 09/28/2022 
Download report in PDF pdf
Principal Investigator/Affiliation:   Miljkovic, Nenad  Ph.D. / University of Illinois, Urbana-Champaign 
Address:  Department of Mechanical Science and Engineering 
105 S Mathews Ave, 2136 Mechanical Engineering Laboratory 
Urbana , IL 61801-2924 
Email: nmiljkov@illinois.edu 
Phone: 617-981-9247  
Congressional District: 13 
Web:  
Organization Type: UNIVERSITY 
Organization Name: University of Illinois, Urbana-Champaign 
Joint Agency:  
Comments:  
Co-Investigator(s)
Affiliation: 
Yazdani, Miad  Ph.D. United Technologies Corporation 
Key Personnel Changes / Previous PI: None to report.
Project Information: Grant/Contract No. 80NSSC22K0294 
Responsible Center: NASA GRC 
Grant Monitor: Chao, David  
Center Contact: 216-433-8320 
david.f.chao@nasa.gov 
Unique ID: 14803 
Solicitation / Funding Source: 2020 Physical Sciences NNH20ZDA012N: Fluid Physics. Appendix A 
Grant/Contract No.: 80NSSC22K0294 
Project Type: FLIGHT,GROUND 
Flight Program: ISS 
No. of Post Docs:
No. of PhD Candidates:
No. of Master's Candidates:
No. of Bachelor's Candidates:
No. of PhD Degrees:
No. of Master's Degrees:
No. of Bachelor's Degrees:
Program--Element: FLUID PHYSICS--Fluid physics 
Flight Assignment/Project Notes: ISS

Task Description: Cryogenic chilldown governs initial stages of cryogen transport. Chilldown involves complicated hydrodynamic and thermal interactions between the liquid, vapor, and channel wall. Large initial temperature differences between the walls and the cryogen create rapid evaporation and large pressure and temperature fluctuation. Although work has attempted to identify transient flow boiling regimes, local surface temperatures, and heat fluxes, chilldown remains poorly understood due to the lack of experimental techniques capable of attaining high spatio-temporal resolution in both optical and infrared (IR) spectra. Furthermore, a lack of computational methods exists which can predict transient flow boiling and chilldown for a variety of length and time scales, and working fluid and system geometries.

Here, we propose a collaborative effort between the University of Illinois, Urbana-Champaign (UIUC) and Raytheon Technologies (RTX) to develop fundamental understanding of chilldown using complementary high-fidelity experiments and computations. Internal flow pattern variations ranging from the film, transition, nucleate, to convection flow boiling using FC-72 and liquid nitrogen (LN2) in NASA relevant aluminum and stainless steel tubes, will be studied. We will use in-liquid endoscopy to study in-situ quench front propagation during FC-72 and LN2 flow boiling. The synchronous use of internal optical and external IR visualization will enable the gaining of a rigorous understanding of the thermal-fluidic behavior occurring in the near-wall region during chilldown and transient flow boiling. The obtained parameters, such as the quench front propagation rate and the temperature and heat flux distributions near the quench front, will then be used to validate high-fidelity computations. The computational framework at RTX leverages the established foundation that is capable of predicting the thermal and hydrodynamic behavior of multiphase flows in convective boiling and condensation regimes. The multiple scales associated with chilldown and two-phase flow boiling will be addressed through a combination of the previously developed Direct Numerical Simulation (DNS) approach for the nucleation near the wall, the Large Eddy Simulation (LES) formulation for the macroscopic transport in the core, and a novel coupling scheme for transporting the information across these scales. While the inherent transient phenomena such as solid condition, nucleation, and regime transition are an integral part of this framework, the model will be modified to allow transient boundary and operating conditions due to the operation of the tank during chilldown. The simulation will provide highly resolved information on the thermal and flow characteristics of two-phase cryogenic flow during the chilldown process and particularly the transient evolution of the flow regime during boiling. The model predictions will continually be validated against the high-fidelity experimental measurements over a range of test conditions. The work is broken down into tasks, which are briefly defined by:

1) Experimental analysis of transient heat transfer and pressure fluctuation during chilldown in Earth gravity with FC-72; 2) Integration of synchronous optical and IR visualization of chilldown with FC-72 and LN2 in Earth gravity for a variety of conditions including tube material, tube size, pressure difference, initial system temperature, and cryogen flow rate; 3) Simulations of transient flow boiling and chilldown in Earth gravity with FC-72 in order to provide physical insight on how the flow regime and boiling regime evolve over the course of chilldown; and 4) FC-72 flow boiling tests in microgravity with simulation validation.

The outcomes of the on-Earth experiments will guide testing in microgravity on the Flow Boiling and Condensation Experiment (FBCE) on the International Space Station (ISS) to better understand the time-varying system pressure and temperatures during the cryogenic propellant transfer process.

Research Impact/Earth Benefits: Cryogenic chilldown governs initial stages of cryogen transport. Flow pattern variation and quench front propagation are crucial for analyzing and understanding the mechanism of chilldown.

Task Progress & Bibliography Information FY2023 
Task Progress: Our project is a joint University of Illinois, Urbana-Champaign (UIUC) and Raytheon Technologies (RTX) - NASA project that aims to develop an understanding of chilldown using high-fidelity experiments and simulations on highly-transient quench front propagation for the purpose of ensuring the efficient and safe utilization of cryogenic fluids during transfer under microgravity conditions.

The specific tasks are: Year 1: FC-72 Experiments and Simulations in Earth Gravity Year 2: Synchronous Optical and Infrared (IR) Visualization using FC-72 in Earth Gravity Year 3: Liquid nitrogen (LN2) Chilldown Experiments and Simulations in Earth Gravity Year 4: FC-72 Experiments and Simulations in Microgravity (International Space Station - Flow Boiling and Condensation Experiment / ISS - FBCE) Year 5: FBCE Data Analysis, Model Validation, and Computational Framework Editing

The summary of the Year 1 contributions from the Principal Investigator Institution and Co-Investigator Institution are stated below.

In this reporting year, the work on terrestrial experiments and microgravity experiments moved forward as planned. We designed the flow boiling setup for terrestrial chilldown experiments with FC-72 and LN2. This was done based on the scientific problem and the test matrices in the proposed proposal and we have completed the assembly of the loop for FC-72 so far. In addition, we have confirmed our collaboration with Case Western Reserve University (CWRU) on the science requirement document (SRD) in May 2022 and have submitted the summary list and the first draft of the SRD in July 2022.

The first phase of the computational portion of this work focused on validation of the convective boiling model against previously obtained experimental data obtained at UIUC. The multiscale approach developed and integrated into the high-fidelity convective boiling framework exploits the separation of length and time scales associated with nucleation and convection with the use of coupling between the nucleation and convection frameworks. The approach provides a practical path towards predictive simulation of convective flow boiling due to the fact that Large Eddy Simulation (LES) models are more amenable in terms of resolution requirement. The convection characteristics, hydrodynamics and thermal, are resolved in what is henceforth referred to as the LES model. However, the reduced resolution and inability of LES models to properly capture the near-wall physics prohibit a full representation of nucleation at the wall, and therefore, a coupling strategy will be used to model the interaction of nucleation at the wall and convection in the core. In this approach, the nucleation behavior is characterized in what is henceforth referred to as the Direct Numerical Simulation (DNS) model of pool boiling. This approach allows for the prediction of hydrodynamic and thermal characteristics of convective flow boiling at large Reynolds numbers at a modest computational cost.

Bibliography: Description: (Last Updated: 09/29/2022) 

Show Cumulative Bibliography
 
Abstracts for Journals and Proceedings Zhang J, Li J, Miljkovic N. "Effects of tube thermal properties on FC-72 line chilldown during low Reynolds number flows." 38th Annual Meeting of the American Society for Gravitational and Space Research, Houston, TX, November 9-12, 2022.

Abstracts. 38th Annual Meeting of the American Society for Gravitational and Space Research, Houston, TX, November 9-12, 2022. , Nov-2022

Project Title:  High-Fidelity Experiments and Computations of Transient Two-Phase Flow for Understanding Cryogenic Propellant Tank Transfer Reduce
Images: icon  Fiscal Year: FY 2022 
Division: Physical Sciences 
Research Discipline/Element:
Physical Sciences: FLUID PHYSICS--Fluid physics 
Start Date: 11/30/2021  
End Date: 11/29/2026  
Task Last Updated: 01/20/2022 
Download report in PDF pdf
Principal Investigator/Affiliation:   Miljkovic, Nenad  Ph.D. / University of Illinois, Urbana-Champaign 
Address:  Department of Mechanical Science and Engineering 
105 S Mathews Ave, 2136 Mechanical Engineering Laboratory 
Urbana , IL 61801-2924 
Email: nmiljkov@illinois.edu 
Phone: 617-981-9247  
Congressional District: 13 
Web:  
Organization Type: UNIVERSITY 
Organization Name: University of Illinois, Urbana-Champaign 
Joint Agency:  
Comments:  
Co-Investigator(s)
Affiliation: 
Yazdani, Miad  Ph.D. United Technologies Corporation 
Project Information: Grant/Contract No. 80NSSC22K0294 
Responsible Center: NASA GRC 
Grant Monitor: Chao, David  
Center Contact: 216-433-8320 
david.f.chao@nasa.gov 
Unique ID: 14803 
Solicitation / Funding Source: 2020 Physical Sciences NNH20ZDA012N: Fluid Physics. Appendix A 
Grant/Contract No.: 80NSSC22K0294 
Project Type: FLIGHT,GROUND 
Flight Program: ISS 
No. of Post Docs:  
No. of PhD Candidates:  
No. of Master's Candidates:  
No. of Bachelor's Candidates:  
No. of PhD Degrees:  
No. of Master's Degrees:  
No. of Bachelor's Degrees:  
Program--Element: FLUID PHYSICS--Fluid physics 
Flight Assignment/Project Notes: ISS

Task Description: Cryogenic chilldown governs initial stages of cryogen transport. Chilldown involves complicated hydrodynamic and thermal interactions between the liquid, vapor, and channel wall. Large initial temperature differences between the walls and the cryogen create rapid evaporation and large pressure and temperature fluctuation. Although work has attempted to identify transient flow boiling regimes, local surface temperatures, and heat fluxes, chilldown remains poorly understood due to the lack of experimental techniques capable of attaining high spatio-temporal resolution in both optical and infrared (IR) spectra. Furthermore, a lack of computational methods exists which can predict transient flow boiling and chilldown for a variety of length and time scales, and working fluid and system geometries.

Here, we propose a collaborative effort between the University of Illinois, Urbana-Champaign (UIUC) and Raytheon Technologies (RTX) to develop fundamental understanding of chilldown using complementary high-fidelity experiments and computations. Internal flow pattern variations ranging from the film, transition, nucleate, to convection flow boiling using FC-72 and liquid nitrogen (LN2) in NASA relevant aluminum and stainless steel tubes, will be studied. We will use in-liquid endoscopy to study in-situ quench front propagation during FC-72 and LN2 flow boiling. The synchronous use of internal optical and external IR visualization will enable the gaining of a rigorous understanding of the thermal-fluidic behavior occurring in the near-wall region during chilldown and transient flow boiling. The obtained parameters, such as the quench front propagation rate and the temperature and heat flux distributions near the quench front, will then be used to validate high-fidelity computations. The computational framework at RTX leverages the established foundation that is capable of predicting the thermal and hydrodynamic behavior of multiphase flows in convective boiling and condensation regimes. The multiple scales associated with chilldown and two-phase flow boiling will be addressed through a combination of the previously developed Direct Numerical Simulation (DNS) approach for the nucleation near the wall, the Large Eddy Simulation (LES) formulation for the macroscopic transport in the core, and a novel coupling scheme for transporting the information across these scales. While the inherent transient phenomena such as solid condition, nucleation, and regime transition are an integral part of this framework, the model will be modified to allow transient boundary and operating conditions due to the operation of the tank during chilldown. The simulation will provide highly resolved information on the thermal and flow characteristics of two-phase cryogenic flow during the chilldown process and particularly the transient evolution of the flow regime during boiling. The model predictions will continually be validated against the high-fidelity experimental measurements over a range of test conditions. The work is broken down into tasks, which are briefly defined by:

1) Experimental analysis of transient heat transfer and pressure fluctuation during chilldown in Earth gravity with FC-72; 2) Integration of synchronous optical and IR visualization of chilldown with FC-72 and LN2 in Earth gravity for a variety of conditions including tube material, tube size, pressure difference, initial system temperature, and cryogen flow rate; 3) Simulations of transient flow boiling and chilldown in Earth gravity with FC-72 in order to provide physical insight on how the flow regime and boiling regime evolve over the course of chilldown; and 4) FC-72 flow boiling tests in microgravity with simulation validation.

The outcomes of the on-Earth experiments will guide testing in microgravity on the Flow Boiling and Condensation Experiment (FBCE) on the International Space Station (ISS) to better understand the time-varying system pressure and temperatures during the cryogenic propellant transfer process.

Research Impact/Earth Benefits: Cryogenic chilldown governs initial stages of cryogen transport. Flow pattern variation and quench front propagation are crucial for analyzing and understanding the mechanism of chilldown.

Task Progress & Bibliography Information FY2022 
Task Progress: New project for FY2022.

Bibliography: Description: (Last Updated: 09/29/2022) 

Show Cumulative Bibliography
 
 None in FY 2022