Numerical Study on Dynamic Stall of Low Reynolds Number Flow Around Boom Mounted U-Tail of FARIDUAV

Emad Hasani Malekshah
Emad Hasani Malekshah M.Sc. of Mechanical Engineering
Mofid Gorji-Bandpy
Mofid Gorji-Bandpy
Imam Hossein University Imam Hossein University

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Numerical Study on Dynamic Stall of Low Reynolds Number Flow Around Boom Mounted  U-Tail of FARIDUAV

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Abstract

This study focuses on tail aerodynamic modeling with CFD simulation of an experimental unmanned aerial vehicle (UAV) in horizontal and vertical section separately. This aircraft with special capabilities has moderate maneuver performance, and predicting the aerodynamic behavior requires knowing that when dynamic stall will occur even in tail. The unsteady nature of the flow field around UAV tail, and the configuration of the generated lift and drag forces must be understood in order to optimize the comfort control system. As a result, flow around the tail and trailing-edge separation of elevator and rudder in horizontal and vertical tail at low Reynolds number with special angle of attack has been simulated .Finally, a custom threecomponent force balance for measuring lift, drag and moment is described in detail. The results indicate that maximum allowable angles of deflection are about 13 and 17 degree in horizontal and vertical tail, respectively. Moreover, each 1degree of deflection decreases almost 0.35 degree horizontal tail stall angle.

References

26 Cites in Article
  1. Dyke Weatherington,Allen Wilson (2005). The Office of the Secretary of Defense (OSD) Unmanned Aerial Vehicles (UAV) Common Mission Planning Architecture (CMPA)- An Overview.
  2. Avi Abershitz,David Penn,Amit Levy,Aviv Shapira,Zvi Shavit,Shlomo Tsach (2005). IAI's Micro / Mini UAV Systems - Development Approach.
  3. D Kubo,S Suzuki,T Kagami (2006). Development of experimental small UAV equipped with cellular phone data link system.
  4. A Ollero,J Ferruz,F Caballero,S Hurtado,L Merino (2004). Motion compensation and object detection for autonomous helicopter visual navigation in the COMETS system.
  5. J Lejot,C Delacourt,H Piégay,T Fournier,M‐l. Trémélo,P Allemand (2007). Very high spatial resolution imagery for channel bathymetry and topography from an unmanned mapping controlled platform.
  6. Chris Hugenholtz,Ken Whitehead,Owen Brown,Thomas Barchyn,Brian Moorman,Adam Leclair,Kevin Riddell,Tayler Hamilton (2013). Geomorphological mapping with a small unmanned aircraft system (sUAS): Feature detection and accuracy assessment of a photogrammetrically-derived digital terrain model.
  7. Chi Yuan,Youmin Zhang,Zhixiang Liu (2015). A survey on technologies for automatic forest fire monitoring, detection, and fighting using unmanned aerial vehicles and remote sensing techniques.
  8. C Cuerno-Rejado,R Martinez-Val (2011). Unmanned Aircraft Systems in the Civil Airworthiness Regulatory System: A Case Study.
  9. J Torres-Sánchez,F López-Granados,J Peña (2015). An automatic object-based method for optimal thresholding in UAV images: Application for vegetation detection in herbaceous crops.
  10. G Salvo,L Caruso,A Scordo (2014). Urban traffic analysis through an UAV.
  11. J Perry,A Mohamed,B Johnson,R Lind (2008). Estimating angle of attack and sideslip under high dynamics on small UAVs.
  12. D Rao,H Tang,T Go (2015). A parametric study of fixed-wing aircraft perching maneuvers.
  13. H Horton (1968). Laminar separation bubbles in two and three dimensional incompressible flow.
  14. Laura Pauley,Parviz Moin,William Reynolds (1990). The structure of two-dimensional separation.
  15. W Phillips,A Hansen,W Nelson (2006). Effects of Tail Dihedral on Static Stability.
  16. M Chandrasekhara,M Wilder (2003). Heat-flux gauge studies of compressible dynamic stall.
  17. J Ekaterinaris,F Menter (1994). Computation of oscillating airfoil flows with one-and two-equation turbulence models.
  18. (1993). Transition effects on compressible dynamic stall of transiently pitching airfoils.
  19. Miguel Visbal (2011). Numerical Investigation of Deep Dynamic Stall of a Plunging Airfoil.
  20. W Mccroskey,L Carr,K Mcalister (1981). Dynamic stall experiments on oscillating airfoils.
  21. Iman Sadeghzadeh,Youmin Zhang (2013). Actuator fault-tolerant control based on Gain-Scheduled PID with application to fixed-wing Unmanned Aerial Vehicle.
  22. Gabriel Weymouth,Robert Wilson,Frederick Stern (2005). RANS Computational Fluid Dynamics Predictions of Pitch and Heave Ship Motions in Head Seas.
  23. A Sanchez-Caja,P Rautaheimo,T Siikonen (2000). Simulation of incompressible viscous flow around a ducted propeller using a RANS equation solver.
  24. F Menter (1994). Two-equation eddy-viscosity turbulence models for engineering applications.
  25. Christopher Rumsey (2010). Compressibility Considerations for k-w Turbulence Models in Hypersonic Boundary-Layer Applications.
  26. Marshall Bern,Paul Plassmann (2000). Mesh Generation.

Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Emad Hasani Malekshah. 2018. \u201cNumerical Study on Dynamic Stall of Low Reynolds Number Flow Around Boom Mounted U-Tail of FARIDUAV\u201d. Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 17 (GJRE Volume 17 Issue A7).

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords
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GJRE-A Classification FOR Code: 290501
Version of record

v1.2

Issue date
January 22, 2018

Language
en
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Numerical Study on Dynamic Stall of Low Reynolds Number Flow Around Boom Mounted U-Tail of FARIDUAV

Emad Hasani Malekshah
Emad Hasani Malekshah <p>Imam Hossein University</p>
Mofid Gorji-Bandpy
Mofid Gorji-Bandpy

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