ANALYSIS OF DEVICES USED IN AERODYNAMIC TESTING

Annotasiya

Aerodynamic testing plays a critical role in modern automotive engineering, enabling accurate analysis of vehicle airflow behavior and drag coefficients. To simulate real-world conditions and validate computational models, specialized devices are employed in wind tunnels and laboratory environments. This study examines the key components involved in aerodynamic testing, including scaled car models, wind tunnels, smoke generators, force measurement systems, and digital sensors. The objective is to analyze the efficiency, accuracy, and integration of these devices in experimental procedures. Through this analysis, the study provides insights into optimizing testing methodologies to achieve better precision in aerodynamic design and development.

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Annotasiya

Aerodynamic testing plays a critical role in modern automotive engineering, enabling accurate analysis of vehicle airflow behavior and drag coefficients. To simulate real-world conditions and validate computational models, specialized devices are employed in wind tunnels and laboratory environments. This study examines the key components involved in aerodynamic testing, including scaled car models, wind tunnels, smoke generators, force measurement systems, and digital sensors. The objective is to analyze the efficiency, accuracy, and integration of these devices in experimental procedures. Through this analysis, the study provides insights into optimizing testing methodologies to achieve better precision in aerodynamic design and development.


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ANALYSIS OF DEVICES USED IN AERODYNAMIC TESTING

Ergashev Dostonbek Pratovich

Assistant, Andijan State Technical Institute

Abstract:

Aerodynamic testing plays a critical role in modern automotive engineering, enabling

accurate analysis of vehicle airflow behavior and drag coefficients. To simulate real-world

conditions and validate computational models, specialized devices are employed in wind tunnels

and laboratory environments. This study examines the key components involved in aerodynamic

testing, including scaled car models, wind tunnels, smoke generators, force measurement

systems, and digital sensors. The objective is to analyze the efficiency, accuracy, and integration

of these devices in experimental procedures. Through this analysis, the study provides insights

into optimizing testing methodologies to achieve better precision in aerodynamic design and

development.

Keywords:

Aerodynamics, wind tunnel, drag force, smoke generator, force sensor, scaled model,

automotive testing

1. Introduction

The pursuit of fuel efficiency, high performance, and environmental sustainability has directed

automotive research toward optimizing aerodynamics. Aerodynamic testing, as a vital aspect of

vehicle development, provides engineers with data to evaluate airflow, drag, lift, and other forces

acting on a vehicle in motion. While computational fluid dynamics (CFD) offers theoretical

insights, physical experiments remain indispensable for validation.
In Uzbekistan and other developing automotive markets, interest in establishing experimental

aerodynamic laboratories has increased. This research focuses on analyzing the function and

construction of experimental devices used in aerodynamic testing, particularly in the context of

scaled car models in wind tunnel environments. The goal is to enhance accuracy and reduce

design iteration costs during vehicle development.

2. Methods

2.1. Overview of the Experimental SetupThe experimental system for aerodynamic testing

typically consists of:
A closed or open-circuit wind tunnel.
Scaled-down automobile models (1:10 or 1:5 scale).
A smoke generator and laser sheet for visualizing airflow.
Force-measuring platform with multi-axis load cells.
High-speed camera or sensor array for data collection.
2.2. Construction of the Wind TunnelThe wind tunnel used in this study was a subsonic, open-

circuit tunnel constructed from durable acrylic and aluminum profiles. A centrifugal fan powered


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by a 2.2 kW electric motor generated controlled airflow. The test section measured 300 mm x

300 mm x 700 mm, with a honeycomb mesh to ensure laminar flow.
2.3. Smoke Visualization and Flow AnalysisTo analyze airflow over the car model, a smoke

generator with glycol-based fluid was utilized. A laser sheet illuminated the flow, and a high-

speed camera recorded the behavior of smoke lines. This helped in identifying flow separation,

vortices, and laminar-to-turbulent transitions.

Figure 1. Schematic of a closed-circuit wind tunnel with an open test section. 1 – adjustable

blades, 2 – return channel, 3 – turning vanes, 4 – settling chamber, 5 – nozzle, 6 – test section, 7

– annular diffuser, 8 – diffuser, 9 – fan, 10 – transition section, 11 – fan group supports, 12 –

electric motor
2.4. Scaled Model and Mounting SystemA 1:10 scale model of a compact vehicle was produced

using 3D printing technology. It was mounted on a low-friction platform connected to a load cell

system that recorded drag and lift forces. The model included interchangeable components

(spoilers, diffusers, etc.) to study their effects on drag.
2.5. Data Acquisition and SensorsThe force measuring system used digital strain gauge sensors

connected to a microcontroller with real-time data logging. Calibration was performed using

known weights. Airspeed was measured with a hot-wire anemometer, and temperature and

pressure were logged to account for air density variations.

3. Results

3.1. Drag Force MeasurementThe system successfully measured drag forces within a ±3%

accuracy range. The baseline drag coefficient (Cd) for the scaled model was calculated to be 0.36,

closely matching computational predictions.
3.2. Effectiveness of Flow VisualizationSmoke streamlines clearly revealed turbulent wake

regions behind the model and flow separation over curved surfaces. Addition of aerodynamic

elements such as a rear spoiler reduced wake turbulence and slightly lowered drag.
3.3. Sensor Response and Data PrecisionForce sensors demonstrated high stability and

repeatability. Data acquisition intervals of 0.1 seconds allowed detailed dynamic analysis of

force fluctuations.
3.4. Limitations ObservedSome challenges included smoke diffusion in high-speed flow, minor

model vibrations, and the need for precise alignment of the model within the test section. These

were partially mitigated by structural reinforcements and flow straighteners.


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Figure 2. Pressure distribution in the wind tunnel circuit. a – static pressure, b – total pressure, 1

– transition section, 2 – turning vane, 3 – return channel, 4 – settling chamber with honeycomb, 5

– nozzle, 6 – test section with model, 7 – diffuser

4. Discussion

The experimental analysis confirms that cost-effective aerodynamic test setups can yield

valuable data for vehicle design improvements. The use of scaled models, when constructed and

calibrated properly, enables close approximation of full-scale behavior. Integrating smoke

visualization techniques allows intuitive interpretation of complex airflow patterns, which is

essential for engineering decision-making.
Force sensors and data loggers proved effective for quantitative evaluation, although their

precision depends on structural stability and environmental conditions. The modular design of

the testing platform permits the study of various aerodynamic modifications efficiently.
Comparison with CFD results revealed a strong correlation, reinforcing the validity of the

experimental approach. Further improvements could involve using wind tunnels with automated

velocity control and integrating AI-based flow analysis tools.

5. Conclusion

This study highlights the feasibility and effectiveness of using scaled-down aerodynamic testing

setups in academic and industrial research. The integration of smoke visualization, precise sensor

technology, and modular vehicle models provides a robust platform for analyzing aerodynamic

forces and flow behavior. These devices, when combined, contribute significantly to reducing

the time and cost of vehicle aerodynamic optimization. Expanding such testing facilities in

Uzbekistan’s technical universities could foster innovation in vehicle design and support the

domestic automotive industry.

References

1.Katz J. Race Car Aerodynamics: Designing for Speed. – Cambridge: Bentley Publishers, 2016.

– 304 p.
2.Hucho W.H. Aerodynamics of Road Vehicles. – Warrendale: SAE International, 1998. – 420 p.
3.Barnard R.H. Road Vehicle Aerodynamic Design. – Bedford: Mechaero Publishing, 2009. –

380 p.
4.Pope A., Goin L. High-Speed Wind Tunnel Testing. – New York: John Wiley & Sons, 1978. –

420 p.


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5.Anderson J.D. Fundamentals of Aerodynamics. – New York: McGraw-Hill Education, 2010. –

1120 p.
6. Allah A. A., Mulyanto T. Analisis Aerodinamika Untuk Desain Mobil Listrik Jenis Kargo

Mini // Scientific Journal of Mechanical Engineering Kinematika. – 2025. – T. 10. – No. 1. – pp.

33-47.
7.Ergashev D. CFD and experimental testing in vehicle aerodynamics //International Journal of

Artificial Intelligence. – 2025. – T. 1. – No. 4. – pp. 801-806.
8.Qayumov B. A., Ergashev D. P. Miniven tipidagi avtomobil kuzaviga havoning qarshilik

kuchini aniqlash //Research and Education.-2023/-T.
9. Kayumov B. A., Ergashev D. P. Analysis of the air force of cylinders and cones in the virtual

test program. – 2022.

Bibliografik manbalar

Katz J. Race Car Aerodynamics: Designing for Speed. – Cambridge: Bentley Publishers, 2016. – 304 p.

Hucho W.H. Aerodynamics of Road Vehicles. – Warrendale: SAE International, 1998. – 420 p.

Barnard R.H. Road Vehicle Aerodynamic Design. – Bedford: Mechaero Publishing, 2009. – 380 p.

Pope A., Goin L. High-Speed Wind Tunnel Testing. – New York: John Wiley & Sons, 1978. – 420 p.

Anderson J.D. Fundamentals of Aerodynamics. – New York: McGraw-Hill Education, 2010. – 1120 p.

Allah A. A., Mulyanto T. Analisis Aerodinamika Untuk Desain Mobil Listrik Jenis Kargo Mini // Scientific Journal of Mechanical Engineering Kinematika. – 2025. – T. 10. – No. 1. – pp. 33-47.

Ergashev D. CFD and experimental testing in vehicle aerodynamics //International Journal of Artificial Intelligence. – 2025. – T. 1. – No. 4. – pp. 801-806.

Qayumov B. A., Ergashev D. P. Miniven tipidagi avtomobil kuzaviga havoning qarshilik kuchini aniqlash //Research and Education.-2023/-T.

Kayumov B. A., Ergashev D. P. Analysis of the air force of cylinders and cones in the virtual test program. – 2022.