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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Bibliographic Details
Published inResearch and science today Vol. 19; no. 1; pp. 45 - 53
Main Author Corpodean, Mircea
Format Journal Article
LanguageEnglish
Published Targu-Jiu Research and Science Today 01.04.2020
University Constantin Brancusi of Târgu-Jiu
Subjects
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
XFLR5
ALOUETTE III
QBLADE
ROTOR
HELICOPTER
ROTARY WINGS
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Summary: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.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:2247-4455
2285-9632
DOI:10.38173/RST.2020.19.1.4:45-53