Helicopter Fuselage Drag ─ Combined Computational Fluid Dynamics and Experimental Studies

In this paper, wind tunnel experiments are combined with Computational Fluid Dynamics (CFD) aiming to analyze the aerodynamics of realistic fuselage con¦gurations. A development model of the ANSAT aircraft and an early model of the AKTAI light helicopter were employed. Both models were tested at the subsonic wind tunnel of KNRTU-KAI for a range of Reynolds numbers and pitch and yaw angles. The force balance measurements were complemented by particle image velocimetry (PIV) investigations for the cases where the experimental force measurements showed substantial unsteadiness. The CFD results were found to be in fair agreement with the test data and revealed some §ow separation at the rear of the fuselages. Once con¦dence on the CFD method was established, further modi¦cations were introduced to the ANSAT-like fuselage model to demonstrate drag reduction via small shape changes

Analytical and Experimental Study of the Integral Aerodynamic Characteristics of Low-Wind Turbines

This work presents experimental and analytical results for a horizontal axis wind turbine designed for operation at low wind speeds. This is dictated by the need to develop wind turbine farms at remote areas where average annual wind speeds are below 7 m/s. The key idea behind the proposed concept is the use a two-element blade. The relative position of the elements is optimized for performance. A closed-circuit, low-speed wind tunnel with open test section is used for a set of measurements on a simple wind turbine with blades made out of the CLARCK Y section without any blade twist. The experimental data is compared with results from the literature in Figure 1 [1] where the efficiency of various wind turbine types is also presented. The results suggest that good efficiencies can be obtained even at low wind speeds if the two lifting elements of the blade are positioned in an optimal way. In addition to the experimental work, an analytical method has also been developed for flapped-blades wind turbines based on the blade element momentum approach. Experimental and analytical studies suggest that the wind turbine with flapped blades design is a sound concept, and can offer a realistic alternative to conventional horizontal-axis wind turbines because of its good power efficiency at low tip speed ratios. This also means that this wind turbine has low noise level due to its lower tip speed. The proposed configuration achieves the best performance at wind speeds of 4- 7 m/s and is therefore suitable for installation at low-wind fields

Analytical and experimental study of the integral aerodynamic characteristics of low-speed wind turbines

This paper proposes a new wind turbine concept suitable for low-speed winds. The design is studied using a combination of wind-tunnel experimentation and aerodynamic theory. After processing the experimental results, and after comparison with theory, the optimal conditions for the operation of the turbine are identified. Experimental and theoretical results suggest that the design offers a realistic alternative to conventional horizontal axis wind turbines. In addition, the proposed turbine has good power efficiency at low wind speeds, and is suitable for deployment in areas not yet favoured by wind farm developers

Helicopter Drag Fuselage- Combined CFD and Experimental Studies

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