Expertise in CFD and External & Internal Aero (Subsonic to Hypersonic Regime). The ideal candidate will have a deep understanding of gas dynamics and shock interactions, aerodynamics, and possess excellent problem solving skills to deliver high-quality simulations for various projects. Function as a solution specialist in the field of Computational Fluid Dynamics using simulation tools such as ANSYS FLUENT, Chemkin or Star CCM+, ANSYS CFX.
Key Responsibilities
Perform aerodynamic simulations across subsonic, transonic, supersonic, and hypersonic regimes using CFD tools (e.g., Ansys Fluent) to evaluate external airframe and internal duct/propulsion flow performance.
Analyze complex flow phenomena such as shock formation, expansion waves, separation, and Shockwave–Boundary Layer Interaction, ensuring accurate prediction of pressure, temperature, and heat flux distributions.
Set up and execute CFD models for external flows (wings, fuselage, control surfaces) and internal flows (intakes, nozzles, ducts), applying appropriate boundary conditions, compressibility effects, and gas dynamic principles.
Apply advanced turbulence models — RANS, LES, DES, or hybrid methods — and justify their selection based on flow regime, Reynolds number,and accuracy requirements.
Generate high-quality meshes for complex geometries using structured, unstructured, or hybrid approaches, ensuring proper near-wall resolution (y⁺ control) and grid independence for reliable aerodynamic predictions.
Conduct 6DOF dynamic simulations using dynamic and overset meshes to study vehicle motion, stability, and control behaviour during free-flight or moving-bodyscenarios.
Post-process and analyse CFD results, extracting aerodynamic coefficients (Cl, Cd, Cm), flow visualization plots (Mach contours, Cp distributions), and force/moment data for design evaluation and optimization.
Collaborate with multidisciplinary teams (structures, thermal, propulsion) by providing aerodynamic loads, surface pressures, and heat flux data for coupled simulations and integrated performance analysis.
Automate workflows and data analysis using Python or scripting tools for mesh generation, solver execution, and result processing to improve efficiency and repeatability.
Document and communicate findings through detailed technical reports, validation studies, and design recommendations to support airframe, propulsion, and system-level development efforts
Requirements
Required Skills:
Perform aerodynamic simulations across subsonic to hypersonic flow regimes.
Analyze external flows over airframes and internal flows through ducts, intakes, and propulsion systems.
Knowledge of Shockwave Boundary Layer Interaction and Gas Dynamics.
Experience with turbulence modeling (RANS, LES, DES) and mesh generation for complex geometries.
Perform 6DOF Simulations with Dynamic and Overset Mesh.
Knowledge of External & Internal Aero (Subsonic to Hypersonic Regime) Modelling– mandatory.
Strong fundamentals in CFD with Ansys Chemkin knowledge- Preferred.
Aerospace (or) Mechanical with strong knowledge on Combustion simulations.
Knowledge of gas dynamics and shock interactions mandatory
Knowledge of external aerodynamics– mandatory
Basic knowledge of MATLAB for post-processing.
Preferred Skills
Fluent dynamic and overset meshing
Fluent 6DOF UDFs
Fluent external aero best practice
Pressure based and density-based solver’s applicability along with pros & cons.
Low subsonic to hyper-sonic flows. Most of the work is in 0.9 to 5 Mach
Adaptive meshing o Job submission on cluster(Pbs scripts) & RSM
TUI journal utilization for automation of work
Parametric optimization through OptiSLang. Parameterization through space claim and fluent for simultaneous design point runs.
Experience with ANSYS FLUENT/ STAR CCM+ or other commercial CFD software.
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