AERODYNAMIC ANALYSIS OF ALOUETTE III ROTARY WINGS
EVER SINCE THE FIRST MODELS APPEARED, THE HELICOPTER HAS REPRESENTED AND WILL BE A SOLID SUBJECT OF STUDY, ALWAYS BEING A PLACE OF IMPROVEMENT IN ITS TECHNOLOGY WITH THE EVOLUTION OF SCIENCE. IN THIS PAPER I WILL PRESENT SOME IDEAS REGARDING THE AERODYNAMIC PERFORMANCES OF THE BEARING ROTORS, USING...
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Published in | Research and science today Vol. 19; no. 1; pp. 45 - 53 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
Targu-Jiu
Research and Science Today
01.04.2020
University Constantin Brancusi of Târgu-Jiu |
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Abstract | EVER SINCE THE FIRST MODELS APPEARED, THE HELICOPTER HAS REPRESENTED AND WILL BE A SOLID SUBJECT OF STUDY, ALWAYS BEING A PLACE OF IMPROVEMENT IN ITS TECHNOLOGY WITH THE EVOLUTION OF SCIENCE. IN THIS PAPER I WILL PRESENT SOME IDEAS REGARDING THE AERODYNAMIC PERFORMANCES OF THE BEARING ROTORS, USING NUMERICAL SOFTWARE SIMULATIONS BASED ON A SCALE MODEL OF THE SA 316B HELICOPTER. |
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AbstractList | Having received financial backing from the French government, which had taken an official interest in the venture, the earlier design was used as a starting point for a new rotorcraft that would harness the newly developed turboshaft engine; only a few years prior, Joseph Szydlowski, the founder of Turbomeca, had successfully managed to develop the Artouste, a 260 hp (190 kW) single shaft turbine engine derived from his Orédon turbine engine. Changes to the performance characteristics of an airfoil may be made in seconds.The airfoil can be defined using NACA feature or introducing the specific coordinates.Results show an excellent comparison to published wind tunnel data. 3.2.NACA 63A611.5 airfoil analysis Simulation parameters: The magnitude of this force is not constant for a given propeller, but depends on the velocity of the incoming air and the rotational velocity of the propeller itself. [...]tests of propellers usually cover a wide regime of operating conditions.The area under the graph illustrates the efficiency of the propeller The relationship between the wind speed and the rate of rotation of the rotor in characterized by a non-dimensional factor known as Tip speed ratio TSR. ANALYSIS OF MODIFIED ALOUETTE III ROTOR A. 2 Bladed rotor Simulation parameters B.4 Bladed rotor Simulation parameters CONCLUSION The effect of the number of the blades; more blades mean higher lift and efficiency, but for this to happen there must be considered a powerful powerplant and/or a higher fuel consumption The effect of the number of the blades; less blades mean less lift and efficiency, but for this to happen there must be considered a weaker powerplant and/or a lower fuel consumption The airfoil must prefferably have a high critic point to delay the separation of the limit layer. EVER SINCE THE FIRST MODELS APPEARED, THE HELICOPTER HAS REPRESENTED AND WILL BE A SOLID SUBJECT OF STUDY, ALWAYS BEING A PLACE OF IMPROVEMENT IN ITS TECHNOLOGY WITH THE EVOLUTION OF SCIENCE. IN THIS PAPER I WILL PRESENT SOME IDEAS REGARDING THE AERODYNAMIC PERFORMANCES OF THE BEARING ROTORS, USING NUMERICAL SOFTWARE SIMULATIONS BASED ON A SCALE MODEL OF THE SA 316B HELICOPTER. |
Author | Corpodean, Mircea |
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Snippet | EVER SINCE THE FIRST MODELS APPEARED, THE HELICOPTER HAS REPRESENTED AND WILL BE A SOLID SUBJECT OF STUDY, ALWAYS BEING A PLACE OF IMPROVEMENT IN ITS... Having received financial backing from the French government, which had taken an official interest in the venture, the earlier design was used as a starting... |
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SubjectTerms | Aircraft Efficiency Fuel consumption General Reference Works Parameter modification Power Power plants Pressure distribution Propellers Reynolds number Rotary wing aircraft Rotary wings Rotation Simulation Source Material Tip speed Turbine engines Turbines Turboshaft engines Turboshafts Velocity Wind speed Wind tunnels Wings |
Title | AERODYNAMIC ANALYSIS OF ALOUETTE III ROTARY WINGS |
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