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◇ RESEARCH · MONTHLY PROGRESS · +6 PROJECTS

Six projects. One research journey.

Every month, our researchers explore new questions, analyze complex engineering challenges, and uncover insights across aerospace, electric mobility, renewable energy, artificial intelligence, and advanced simulation. This page documents that journey — capturing the milestones, discoveries, and technical progress achieved throughout our ongoing research programs.

MONTHLY RESEARCH PROGRESS ACROSS AEROSPACE, ENERGY, AI & ADVANCED ENGINEERING

◇ TRACKING DISCOVERY THROUGH RESEARCH

Research is not a single breakthrough. It is a continuous process of questioning, testing, analyzing, and refining ideas over time.

Across our six active research programs, each month contributes new findings, simulation results, design improvements, and technical understanding. These progress logs provide a transparent view into how engineering challenges are explored and how solutions gradually emerge through systematic investigation.

 

From aerodynamic optimization and spacecraft propulsion to electric vehicles, hydro power, and AI-driven engineering, every project follows a unique path of discovery.

 

Below you will find a chronological record of monthly achievements, key observations, and research milestones as they unfold throughout each program.

Electric Vehicles

Battery temperature influences safety, lifespan, and performance. Follow our monthly research journey as we investigate nanofluid-based cooling strategies for next-generation electric vehicles.

Jul26

Based on the current study’s analysis, nanofluid performance is sensitive to the sequence of cooling stages rather than just the final temperature. Water+CuO adapts efficiently across successive cooling steps, while Water+Au shows dependency on intermediate conditions before reaching optimal performance. This indicates that cooling history plays a role in nanofluid effectiveness, a factor often overlooked in conventional analysis.

Jun26

Based on the current study’s analysis, transient thermal oscillations are more pronounced in Water and Water+Ag compared to other nanofluids. These fluctuations suggest intermittent heat transfer efficiency during stabilization phases, whereas Water+CuO exhibits smoother transitions. Such transient behavior, though subtle, can influence long-term system reliability.

Apr26

Based on the current study’s analysis, a damping effect introduced by nanoparticles becomes evident. Water+Al₂O₃ shows a gradual thermal response that reduces sharp temperature gradients, acting as a buffer during cooling transitions. This behavior, although less aggressive in cooling rate, helps minimize thermal shock—an aspect often neglected when evaluating peak performance alone.

Mar26

Based on the current study’s analysis, it is observed that nanofluids respond differently under extreme cooling conditions compared to moderate ones. Water+Cu maintains consistent performance even when temperature changes are abrupt, whereas Water+Au and Water+Ag perform better once the system approaches a stable regime. This indicates that some nanofluids are more resilient to rapid thermal disturbances, while others favor steady-state operation.

Feb26

Based on the current study’s analysis, it is evident that nanofluids not only differ in overall efficiency but also in how steadily they manage transitions during C (Thermo-Electric Cooler Temperature) fluctuations. Water+Cu demonstrates strong adaptability, maintaining stable performance across both sharp and mild cooling shifts, whereas Water+Au, though generally efficient, tends to stabilize more slowly, hinting at nanoparticle clustering effects. Water+Ag shows a tendency for quick initial cooling followed by small oscillations, which suggests uneven thermal dispersion under fluctuating loads. In contrast, Water+Al₂O₃ provides a slower but smoother cooling response, making it advantageous in systems where avoiding sudden temperature shocks is critical. A finer detail often overlooked is that water alone not only lags in efficiency but also amplifies temperature swings, creating thermal stress on the system. These subtle differences highlight that beyond conductivity, nanoparticle stability and response time are key in selecting nanofluids for dynamic thermal management.

Subsonic Aircraft

Small changes in wing geometry can create significant aerodynamic advantages. Follow our monthly discoveries as we investigate advanced flap concepts for more efficient subsonic aircraft performance.

Jul26

The data suggests that each feature geometry possesses a narrow operating range where its aerodynamic contribution is most effective. This implies that the performance of wing-attached features is highly dependent on matching geometry to specific operational conditions, rather than relying solely on configurations that maximize peak efficiency.

Jun26

The fillet edge tail, despite lower efficiency values, exhibits a smooth and nearly linear efficiency trend across flap angles. This indicates predictable aerodynamic behavior, which may be advantageous in flight regimes where consistency and controllability are prioritized over maximum efficiency.

Apr26

The partial aerodynamic tail demonstrates small but persistent efficiency oscillations, implying transitional flow behavior around the wing–feature interface. This suggests that partial geometric modifications may introduce complex local flow interactions that do not manifest as large efficiency losses but could influence stability and control response.

Mar26

The analysis indicates that as flap deflection increases, the efficiency gap between different feature geometries gradually narrows. While the full aerodynamic tail initially outperforms the others, the relative advantage diminishes at higher deflections, suggesting that aerodynamic benefits become less geometry-dependent under more aggressive control settings.

Feb26

The analysis reveals that the feature with a full aerodynamic tail shows a steeper efficiency gradient, achieving high values initially but losing performance more rapidly as flap deflection increases, which suggests it is highly effective but sensitive to operational limits. The partial aerodynamic tail demonstrates a gentler efficiency slope, indicating a more balanced response where performance is maintained across a wider range of conditions without sharp drops. The fillet edge tail, despite consistently lower efficiency, exhibits the most uniform trend, with nearly linear changes that imply predictable flow characteristics. These subtle variations emphasize that while maximum efficiency is important, the rate of change and stability of aerodynamic response across flap angles provide equally valuable insights for practical applications.

Hydro Power

Vortex interactions hold untapped potential for improving thrust and energy extraction. Explore our monthly progress as we study contra-rotating propeller systems for advanced hydro power applications.

Jul26

The initial study suggests us that the turbulence intensity mainly affects the ducted tidal turbine having convergence angle below 10 degree. The result also indicates that the variable ‘rpm’, when consider its relationship with the thrust and torque, seems complex and more analysis is needed. The dominating variable and there inter-dependency is yet to find out.

Jun26

The secondary vortex is interacting with the primary vortex near the main blade region from its time of formation and also converging it. Additionally, from the mid region study, the primary vortex pull is non-intact by the region of influence of secondary vortex.

Apr26

The mid-region study shows that the secondary vortex is participating in two different phenomena. Along with the formation of vortex cover, it partially inducing the rotational flow towards the primary vortex. Sustainability of this duel phenomena continue to occur for all energy level of the secondary vortex.

Mar26

The primary vortex remains controlled near the main propeller region and starts bending along the downstream. It could be because: 1. The opposite spin of secondary vortex is destabilizing the center-rotation point of primary vortex or 2. The energy of primary vortex is too high and get space to decapitate when the effect of secondary vortex vanishes. Finally resulting in twisted vortex.

Feb26

Shifting of vortex systems interaction area leads to significant reallocation of maximum thrust region.

Satellite Propulsion

Unlike fixed-wing aircraft, a quadrotor makes lift with several propellers spinning right next to its structure. That creates three-dimensional flow you cannot predict with theory alone.

Jul26

Transient flow analysis identified regions where shock-boundary layer interactions affected expansion efficiency. Preliminary optimization studies suggest that moderate divergence angles may improve thrust generation by reducing flow separation and promoting more uniform exhaust expansion.

Jun26

Additional simulations were performed across varying inlet pressures and nozzle geometries. Results showed that small changes in throat diameter significantly influenced Mach number development, while shock formation became increasingly sensitive to expansion angle at higher pressure ratios.

Apr26

Initial CFD simulations of the micro-thruster nozzle were completed under baseline operating conditions. Early flow visualization revealed the formation of localized high-velocity regions immediately downstream of the throat, indicating efficient acceleration but also suggesting potential expansion losses within the diverging section.

Quad Drone

From propeller downwash to wake development, this research investigates how airflow interacts with drone structures. Explore our monthly findings as we work toward more efficient and stable quadrotor designs.

Jul26

Detailed turbulence analysis identified several recirculation zones beneath the central frame structure during hovering conditions. Early optimization studies suggest that strategic geometric modifications may reduce downwash losses and improve overall thrust efficiency and flight stability.

Jun26

Multiple frame configurations were evaluated to understand how structural geometry affects wake development. Simulations indicated that arm spacing and cross-sectional dimensions play an important role in reducing aerodynamic interference and improving airflow distribution.

Apr26

Baseline quadrotor models were analyzed to study propeller downwash interaction with structural components. Initial findings revealed noticeable airflow disturbances around the drone arms, generating localized turbulence beneath the rotor plane.

AI-driven Engineering Simulation

By combining physics-based simulation with machine learning, we are developing faster and smarter engineering workflows. Discover how our research evolves each month through data, models, and optimization studies.

Jul26

Simulation datasets were generated across multiple operating conditions to establish a foundation for machine learning model development. Initial data analysis confirmed strong relationships between design variables and system performance metrics, supporting the feasibility of predictive modeling.

Jun26

Several machine learning algorithms were trained using simulation-generated data. Early results demonstrated that AI models could predict engineering outcomes with reasonable accuracy while requiring only a fraction of the computational time of full simulations.

Apr26

Simulation datasets were generated across multiple operating conditions to establish a foundation for machine learning model development. Initial data analysis confirmed strong relationships between design variables and system performance metrics, supporting the feasibility of predictive modeling.

Quad Drone

Unlike fixed-wing aircraft, a quadrotor makes lift with several propellers spinning right next to its structure. That creates three-dimensional flow you cannot predict with theory alone.

Jul26

Detailed turbulence analysis identified several recirculation zones beneath the central frame structure during hovering conditions. Early optimization studies suggest that strategic geometric modifications may reduce downwash losses and improve overall thrust efficiency and flight stability.

Jun26

Multiple frame configurations were evaluated to understand how structural geometry affects wake development. Simulations indicated that arm spacing and cross-sectional dimensions play an important role in reducing aerodynamic interference and improving airflow distribution.

Apr26

Baseline quadrotor models were analyzed to study propeller downwash interaction with structural components. Initial findings revealed noticeable airflow disturbances around the drone arms, generating localized turbulence beneath the rotor plane.

◇ JOIN THE RESEARCH JOURNEY

Let's explore the next engineering breakthrough  together.

Behind every monthly finding is a team of researchers asking questions, running simulations, analyzing results, and pushing ideas further than they were the month before. Across aerospace, electric vehicles, renewable energy, artificial intelligence, fluid dynamics, and advanced engineering systems, our research programs provide opportunities to contribute to real-world investigations with measurable impact.

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