Research Articles Issue 1 · 2020 · pp. 45–53 · Issue page

AERODYNAMIC ANALYSIS OF ALOUETTE III ROTARY WINGS

MI
1 Student, “ Henri Coandă” Air Force Academy, Brașov
Received 15 January 2020
Revised 27 January 2020
Accepted 09 March 2020
Available Online 15 March 2020
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 TECHNO LOGY 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 316 B HELICOPTER.
ROTOR XFLR5 QBLADE HELICOPTER ROTARY WINGS ALOUETTE III
The body of this article is intentionally hidden on the public page. Please use the PDF reader or the PDF download for the complete text.
[1]
Vasile, Prisacariu; Elefterie Oliver, Ciuică; Aeronave de şcoală şi antrenament ISBN 978 -606-8356- 35-8,
[2]
Vasile, Prisacariu; The aerodynamic analysis of the profiles for flying wings Journal of Defense Resources Management 4 (1), 211
[3]
Anderson, John David ; (1997). A History of Aerodynamics and its Impact on Flying Machines . New York, NY: Cambridge University Press. ISBN 0-521-45435-2.
[4]
Prouty, Raymond W. ; (2001). Helicopter Performance, Stability, and Control. Krieger Publishing Company Press. ISBN 1-57524-209-5. OCLC 212379050.
[5]
Pope, Stephen B. (2000). Turbulent Flows. Cambridge University Press. ISBN 0 -521-59886-9. OCLC 174790280.
[6]
XFLR5 Guidelines http://www.xflr5.tech/docs/XFLR5_and_Stability_analysis.pdf
[7]
Qblade- Wind turbine design and simulation application https://sourceforge.net/projects/qblade/files/Guidelines/
[8]
Helicopter performance https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/helicopter_flying_handbook/m edia/hfh_ch07.pdf
[9]
Airfoiltools Database https://www.airfoiltools.com/airfoils
[10]
*** Comparison of Aerodynamics Characteristics of NACA 0015
[11]
Technical Manual SA316B, Department of the Army 1996 ISBN 008-1035-08-5
[12]
John D. Anderson Jr. 2007 , Fundamentals of Aerodynamics, Fourth edition ISBN 007-1254-08-0
[13]
Vasile, Prisacariu; Alexandru, Chiril ă; Aerodynamic analysis of helicopter fenestron vertical tail, AFASES 2019 ISSN-L 2247-3173,p. 173-183, DOI: 10.19062/2247-3173.2019.21.24