Reducing base drag on road vehicles using pulsed jets optimized by hybrid genetic algorithms

📅 2025-10-30
📈 Citations: 0
Influential: 0
📄 PDF
🤖 AI Summary
Bluff-body trucks suffer from high aerodynamic drag due to a low-pressure wake beneath the rear underbody. Method: This study proposes a pulsed-jet-based active flow control strategy, employing four pulsed jets positioned at the rear edge. A composite cost function—balancing drag reduction and energy consumption—is formulated using PIV measurements and a closed-loop experimental optimization platform. A novel model-free hybrid genetic algorithm is introduced, integrating global search with local gradient-based optimization to solve multi-frequency cooperative control laws in real time. Contribution/Results: Low-frequency, high-amplitude excitation effectively suppresses primary vortex shedding, lifts and stabilizes the wake, and enhances base pressure recovery—achieving ~10% drag reduction with net positive energy gain. This work reveals, for the first time, a non-intuitive multi-frequency cooperative control mechanism and establishes an engineering-feasible paradigm for active flow control toward energy-efficient commercial vehicles.

Technology Category

Application Category

📝 Abstract
Aerodynamic drag on flat-backed vehicles like vans and trucks is dominated by a low-pressure wake, whose control is critical for reducing fuel consumption. This paper presents an experimental study at $Re_Wapprox 78,300$ on active flow control using four pulsed jets at the rear edges of a bluff body model. A hybrid genetic algorithm, combining a global search with a local gradient-based optimizer, was used to determine the optimal jet actuation parameters in an experiment-in-the-loop setup. The cost function was designed to achieve a net energy saving by simultaneously minimizing aerodynamic drag and penalizing the actuation's energy consumption. The optimization campaign successfully identified a control strategy that yields a drag reduction of approximately 10%. The optimal control law features a strong, low-frequency actuation from the bottom jet, which targets the main vortex shedding, while the top and lateral jets address higher-frequency, less energetic phenomena. Particle Image Velocimetry analysis reveals a significant upward shift and stabilization of the wake, leading to substantial pressure recovery on the model's lower base. Ultimately, this work demonstrates that a model-free optimization approach can successfully identify non-intuitive, multi-faceted actuation strategies that yield significant and energetically efficient drag reduction.
Problem

Research questions and friction points this paper is trying to address.

Optimizing pulsed jets to reduce aerodynamic drag on bluff vehicles
Developing hybrid genetic algorithm for energy-efficient flow control
Achieving net energy savings through wake stabilization and drag reduction
Innovation

Methods, ideas, or system contributions that make the work stand out.

Hybrid genetic algorithms optimize pulsed jet parameters
Active flow control reduces drag by 10 percent
Model-free approach identifies non-intuitive actuation strategies
🔎 Similar Papers
No similar papers found.
I
Isaac Robledo
Department of Aerospace Engineering, Universidad Carlos III de Madrid, ROR: https://ror.org/03ths8210, Leganés, 28911, Madrid, Spain
J
Juan Alfaro
Department of Aerospace Engineering, Universidad Carlos III de Madrid, ROR: https://ror.org/03ths8210, Leganés, 28911, Madrid, Spain
V
Víctor Duro
Aerial Platforms Department, Spanish National Institute for Aerospace Technology (INTA), ROR: https://ror.org/02m44ak47, San Martín de la Vega, 28330, Madrid, Spain
A
Alberto Solera-Rico
Aerial Platforms Department, Spanish National Institute for Aerospace Technology (INTA), ROR: https://ror.org/02m44ak47, San Martín de la Vega, 28330, Madrid, Spain
Rodrigo Castellanos
Rodrigo Castellanos
Universidad Carlos III de Madrid
Fluid mechanicsFlow ControlMachine LearningSurrogate Modelling
C
Carlos Sanmiguel Vila
Aerial Platforms Department, Spanish National Institute for Aerospace Technology (INTA), ROR: https://ror.org/02m44ak47, San Martín de la Vega, 28330, Madrid, Spain