Turbomachinery Engineer - Fluidic Design

Canada Rocket Company

$100K — $120K *
Aerospace & Defense
5 - 7 years of experience
Job Overview by Ladders

Qualifications

  • Bachelor's or graduate degree in mechanical or aerospace engineering with 3-5 years of experience, PhD candidates welcome.
  • Strong expertise in aerodynamics, thermodynamics, and hydrodynamics relevant to high-speed turbomachinery.
  • In-depth knowledge of cavitation, NPSH analysis, and rotor-stator interactions in cryogenic systems.
  • Proficiency in ANSYS and experienced with structured/unstructured meshing techniques in commercial CFD codes.
  • Experience with Siemens NX and ANSYS BladeModeler for geometry development and blade design.
  • Solid programming skills in Python, MATLAB, or FORTRAN for design tools and automation.
  • Hands-on experience correlating CFD with test data for design iterations.

Responsibilities

  • Lead the fluidic design of cryogenic pumps and turbines, covering all design stages from sizing to validation.
  • Define flow path geometry in Siemens NX and develop rotor definitions in ANSYS.
  • Conduct extensive CFD analyses, including steady and transient simulations in various flow conditions.
  • Predict performance characteristics across operational maps, addressing potential mechanical limitations.
  • Investigate off-design behaviors and incorporate findings back into design and system models.
  • Create and maintain preliminary design codes and reduced-order models using Python or MATLAB.
  • Support pre-test predictions and correlate CFD results with actual test data.

Benefits

  • Collaboration with a team of experts in aerospace engineering and turbomachinery.
  • Opportunity to innovate and lead projects critical to aerospace technology.
  • Access to high-performance computing resources for advanced analysis.
  • Involvement in cutting-edge research and development in rocket propulsion systems.
  • Flexibility in work arrangements to support a balanced work-life dynamic.
Full Job Description
About the role

Canada Rocket Company is building the turbomachinery that drives our 700 kN engine. We're looking for a Turbomachinery Engineer - Fluidic Design to lead the analysis, design, and optimization of the rotating machinery at the heart of the engine; pumps: inducers, impellers, diffusers, volutes; turbines: manifolds, nozzles and rotor blades; and the secondary flow systems/axial thrust balancing. You'll own the hydrodynamic and aerodynamic design point, the off-design behaviour, and the secondary circuit using both reduced order modeling and 3D CFD.

What you'll do

  • Lead the fluidic design of cryogenic pumps and hot-side turbines end-to-end, inducers, impellers, diffusers, volutes, turbine manifolds, nozzles and rotors; the secondary flow circuits/axial balancing systems from preliminary sizing through detailed design and validation.
  • Define and refine flow path geometry in Siemens NX and develop blade definitions in ANSYS BladeModeler.
  • Run CFD analyses across the full envelope: steady and transient, single- and multiphase, cavitating inducer flow, supersonic blade rows, and rotor-stator interaction. Use ANSYS Workbench / Fluent / CFX on Linux/HPC.
  • Own performance prediction across the operating map: NPSH margins, head-flow and efficiency curves, blockage and stall limits, tip leakage, secondary flow losses, supersonic nozzle while considering mechanical limitations.
  • Investigate off-design and transient behaviour, start and shutdown transients, throttling, and cycle coupling, and feed the results back into the design and the engine cycle model.
  • Develop and maintain in-house preliminary design codes, reduced-order models, and post-processing tooling in Python, MATLAB, or FORTRAN. Build the workflow, not just the report.
  • Drive pre-test predictions, instrumentation strategy, and post-test correlation for component and full turbopump campaigns. Reconcile CFD with measured data, close the loop, and improve predictive capability for the next build.
  • Work directly with mechanical design, manufacturing, and test to make sure what's analytically optimal is also buildable and inspectable. Push back on geometry that's expensive or risky to produce.
  • Produce the analysis reports, test reports, and design review packages that anchor configuration decisions across the program.

Qualifications

  • Bachelor's degree in mechanical engineering, Aerospace Engineering, or a closely related field, with a minimum of 5 years of relevant experience. A graduate degree with 3 years of experience is equivalent. PhD candidates are also welcome to apply.
  • Strong foundation in aerodynamics, thermodynamics, hydrodynamics, and the principles of high-speed turbomachinery, with the ability to lead the analysis, design, and optimization of inducers, impellers, diffusers and volutes as well as turbines nozzles and rotors in cryogenic and high-temperature environments.
  • Deep working knowledge of cavitation and NPSH analysis, rotor-stator interaction, secondary flow losses, and high-temperature supersonic turbine.
  • High proficiency with commercial CFD codes (ANSYS Workbench / Fluent / CFX), including steady, transient, cavitation, and multiphase modeling. Strong meshing discipline - structured/unstructured, boundary-layer resolution, y+ control, and grid convergence using TurboGrid, ICEM-CFD and other Ansys meshing tools.
  • Fluency with Siemens NX for flow path and assembly geometry, and with ANSYS BladeModeler (or equivalent) for blade definition. Comfortable owning the geometry from concept through CFD without dropping fidelity at the handoff.
  • Solid programming and scripting ability in Python, MATLAB, or FORTRAN for preliminary design tools, reduced-order modelling, post-processing, and automation.
  • Prior exposure to aerospace configuration control and traceability for flight or test hardware.
  • Hands-on experience correlating CFD and analytical predictions with test data - cold-flow, spin, or hot-fire - and using the correlation to drive design iterations.
  • Familiarity with engine cycles (gas generator, staged combustion, expander, etc.), cryogenic propellants, and the reliability constraints of high-speed rotating equipment.
  • Ability to produce clear analysis and test reports and to present results to internal teams and external customers.
  • Fluent English, strong communication skills, and effectiveness in multidisciplinary engineering environments.

Similar Jobs

More Jobs at Canada Rocket Company

More Aerospace & Defense Jobs

Find similar Turbomachinery Engineer - Fluidic Design jobs: