10th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles & SPICES Workshop

Date: December 12-14, 2024 | Venue: Uday Samudra Leisure Beach Hotel, Thiruvananthapuram

SAROD 2024

Theme: Aerodynamics & Aerothermodynamics for Human Rated & Autonomous Aerospace Vehicles

Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD) is a unique international conference which provides a platform to the aero and fluid dynamics community to exchange their thought process on the advancements and progresses made in the fields of aero and fluid dynamics. SAROD 2024 carries forward this legacy and aims to bring together leading aerodynamicists from India and around the world.

Announcements

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10th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles & SPICES Workshop

SAROD 2024 - On December 12-14, 2024 at Uday Samudra Leisure Beach Hotel, Thiruvananthapuram

SPICES (Symposium for Promotion of Indigenous CFD for Engineering Sciences)

Sponsors

Key Topics

  • Aerodynamics of aerospace vehicles and missiles
  • Aerothermodynamics of Human Space Missions
  • Hypersonic and re-entry vehicle aerodynamics
  • Air breathing propulsion and rotorcraft aerodynamics
  • Aerospace vehicle design & multi-disciplinary optimization
  • Wind tunnel testing, Model Design & fabrication and Balance Design
  • Experimental aerodynamic diagnosis techniques
  • CFD techniques, numerical methods, grid generation algorithms
  • Aero thermal design, analysis and testing
  • Internal fluid flows and testing techniques
  • Fluid dynamics of advanced propulsive systems
  • Applied Flight Mechanics and controls
  • Aeroacoustics and unsteady aerodynamics
  • Fluid Structure Interaction and aeroelasticity
  • AI & ML in Aerodynamic Design, Analysis and Testing.
  • Flight dynamics, Multi-Body Separation Dynamics, Parameter Estimation, Trajectory Optimization, Control and Guidance
  • Multi-phase flows, Micro-fluidics and Bio-fluid dynamics.
  • Special purpose testing: Free flight, RTRS, Ballistics range testing, plasma tunnel testing
  • Launch vehicle spent stage recovery, retropropulsion, aerodynamic deceleration, vertical recovery and vertical landing