Air Force Research Laboratory
Multiphase Flow Scientist
Air Force Research Laboratory, Rosamond, California, United States, 93560
Job Overview
This job announcement will be accepting candidate submissions from 16 Sep 2023 to 16 Oct 2024.
The AFRL Combustion Devices Branch within the Rocket Propulsion Division, Aerospace Systems Directorate, seeks to fill a mid-level position at DR-02 or DR-03 levels (depending on qualifications and experience) as Multiphase Flow Scientist. The position is located at the Rocket Test Site in Leuhman Ridge, Edwards AFB, CA.
We are searching for a high-performing, highly-motivated individual with a strong scientific research background on computational multiphase flow physics to become a new member of the Combustion Devices Branch. In this role, you will apply your skills to solve complex scientific problems that will advance our nation’s Rocket Power of Tomorrow.
Position duties include, but are not limited to:
Perform cutting edge, massively parallel numerical simulations of multiphase flow physics of relevance for rocket engines and high-speed systems.
Formulate, implement and demonstrate theoretical and computational multiphase flow models involving turbulence, cryogenics, propellant sprays, propellant flashing, propellant boiloff, detonations, supercritical & transcritical pressures, shock waves, vacuum effects, surface deformation/erosion, solid particulates, conjugate heat transfer, microgravity effects, hydrocarbon fuel/oxidizer combustion kinetics, solid-phase and liquid-phase reactions.
Develop and maintain large-scale, custom-made, non-commercial HPC simulation codes designed for scientific discovery.
Analyze and interpret large amounts of simulation data to inform the design of rocket engines and flight vehicles.
Work closely with our in-house experimental test group and inform hardware design and test campaigns based on simulation results.
Interface with external research organizations, including academia, government agencies, and industry partners.
Required Qualifications
US Citizenship.
Ph.D. degree in Aerospace Engineering, Mechanical Engineering, Chemical Engineering, Applied Physics, or Computational Mathematics from an accredited academic institution. Non-PhD candidates who are close to graduation from their PhD programs will also be considered.
The ability to obtain and maintain a Secret security clearance.
Strong fundamental knowledge of multiphase flow physics and their applications to rocket propulsion or high-speed systems.
Hands-on scientific research experience using High-Performance Computing (HPC) capabilities within the context of multiphase flow physics.
Experience with developing and maintaining parallelized research simulation codes in C++, Fortran, and Python.
Demonstrated experience with code development, simulation data analysis, scientific rigor, physical interpretation, and communication of results to technical audiences via referred journal papers and technical seminars.
This position is an Acquisition Professional Development Program (APDP) position requiring level 1-Foundational, Non-Critical certification in Engineering & Technical Management. The selectee will have 24-months to meet APDP requirements or a waiver must be obtained.
Desired Qualifications
Strong scientific knowledge on current trends in computational multiphase flow physics.
Experience in modern aspects of data science and data-driven modeling.
Experience in performing integrated, full-system simulations.
Knowledge of physicochemical peculiarities associated with cryogens and hypergolic propellants.
Familiarity with practical engineering aspects of rocket engines and high-speed systems.
Genuine interest in working with a diverse team to solve multidisciplinary applied engineering problems and advance the mission of the Air & Space Forces.
Additional Information
Must be able to travel
- Relocation or other incentives may be offered for this position.
Series
0861
#J-18808-Ljbffr
This job announcement will be accepting candidate submissions from 16 Sep 2023 to 16 Oct 2024.
The AFRL Combustion Devices Branch within the Rocket Propulsion Division, Aerospace Systems Directorate, seeks to fill a mid-level position at DR-02 or DR-03 levels (depending on qualifications and experience) as Multiphase Flow Scientist. The position is located at the Rocket Test Site in Leuhman Ridge, Edwards AFB, CA.
We are searching for a high-performing, highly-motivated individual with a strong scientific research background on computational multiphase flow physics to become a new member of the Combustion Devices Branch. In this role, you will apply your skills to solve complex scientific problems that will advance our nation’s Rocket Power of Tomorrow.
Position duties include, but are not limited to:
Perform cutting edge, massively parallel numerical simulations of multiphase flow physics of relevance for rocket engines and high-speed systems.
Formulate, implement and demonstrate theoretical and computational multiphase flow models involving turbulence, cryogenics, propellant sprays, propellant flashing, propellant boiloff, detonations, supercritical & transcritical pressures, shock waves, vacuum effects, surface deformation/erosion, solid particulates, conjugate heat transfer, microgravity effects, hydrocarbon fuel/oxidizer combustion kinetics, solid-phase and liquid-phase reactions.
Develop and maintain large-scale, custom-made, non-commercial HPC simulation codes designed for scientific discovery.
Analyze and interpret large amounts of simulation data to inform the design of rocket engines and flight vehicles.
Work closely with our in-house experimental test group and inform hardware design and test campaigns based on simulation results.
Interface with external research organizations, including academia, government agencies, and industry partners.
Required Qualifications
US Citizenship.
Ph.D. degree in Aerospace Engineering, Mechanical Engineering, Chemical Engineering, Applied Physics, or Computational Mathematics from an accredited academic institution. Non-PhD candidates who are close to graduation from their PhD programs will also be considered.
The ability to obtain and maintain a Secret security clearance.
Strong fundamental knowledge of multiphase flow physics and their applications to rocket propulsion or high-speed systems.
Hands-on scientific research experience using High-Performance Computing (HPC) capabilities within the context of multiphase flow physics.
Experience with developing and maintaining parallelized research simulation codes in C++, Fortran, and Python.
Demonstrated experience with code development, simulation data analysis, scientific rigor, physical interpretation, and communication of results to technical audiences via referred journal papers and technical seminars.
This position is an Acquisition Professional Development Program (APDP) position requiring level 1-Foundational, Non-Critical certification in Engineering & Technical Management. The selectee will have 24-months to meet APDP requirements or a waiver must be obtained.
Desired Qualifications
Strong scientific knowledge on current trends in computational multiphase flow physics.
Experience in modern aspects of data science and data-driven modeling.
Experience in performing integrated, full-system simulations.
Knowledge of physicochemical peculiarities associated with cryogens and hypergolic propellants.
Familiarity with practical engineering aspects of rocket engines and high-speed systems.
Genuine interest in working with a diverse team to solve multidisciplinary applied engineering problems and advance the mission of the Air & Space Forces.
Additional Information
Must be able to travel
- Relocation or other incentives may be offered for this position.
Series
0861
#J-18808-Ljbffr