NUMERICAL INVESTIGATION OF TWO ELEMENT CAMBER MORPHING AIRFOIL IN LOW REYNOLDS NUMBER FLOWS
- Published: 01 Jul 2017 Journal: Journal of Engineering Science and Technology (issn: 1823-4690,
Copyright policy)
- Publisher: Taylor's University
1. Barbarino, S.;Bilgen, O.; Friswell, M.I.;Ajai, R.M.; and Inman, D.J. (2010). A review of morphing aircraft. Journal of Intelligent Material Systems and Structures, 22(9), 823-877.
2. Friswell, M.I. (2014). Morphingaircraft: an improbable dream? Proceedings of the ASME 2014 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Newport, Rhode Island, USA,1-7. [OpenAIRE]
Vasista, S.;Tong, L.; and Wong, K.C. (2012). Realization of morphing wings: amultidisciplinary challenge. Journal of Aircraft, 49(1), 11-28.
4. Poonsong, P. (2004). Design and analysis of a multi-section variable camber wing. MSc. Thesis. University of Maryland, College Park, MD 20742, United States.
Ko, S.H.;Bae, J.S.;and Rho, J.H. (2014). Development of a morphing flap using shape memory alloy actuators: the aerodynamic characteristics of a morphing flap. Smart Materials and Structures, 23(7), 1-21.
Wang, Y. (2015). Development of flexible-rib morphing wing system. M.Sc.
Thesis. University of Toronto, 27 King's College Cir, ON M5S, Canada.
Woods, B.K.S.; Bilgen, O.; and Friswell, M.I. (2014). Wind tunnel testing of the fish bone active camber morphing concept. Journal of Intelligent Material Systems and Structures, 25(7),772-785. [OpenAIRE]
8. Counsil, J.N.N.; and Boulama, K.G. (2013). Low-Reynolds-number aerodynamic performance of NACA 0012 and Selig-Donovan 7003 airfoils. Journal of Aircraft, 50(1), 204-216.
XFLR5 ver. 6.10.04 (2014).
fromhttp://www.xflr5.com/xflr5.htm
10. Selig, M.S.; Deters, R.W.; and Williamson, G.A. (201l). Wind tunnel testing airfoils at low reynolds numbers. 49th AIAA Aerospace Sciences Meeting, Orlando, FL, 1-32.
11. Van Ingen, J.L. (2008). The eN method for transition prediction. Historical review of work at TU Delft. 38thFluid Dynamics Conference and Exhibit, Seattle, Washington, 1-49.
12. Wahidi, R.; and Bridges, D.H. (2009). Experimental investigation of the boundary layer and pressure measurements on airfoil with laminar separation bubbles. 39th AIAA Fluid Dynamics Conference, San Antonia, Texas. [OpenAIRE]
13. Muller, T.J. (1999). Aerodynamic measurements at low Reynolds numbers for fixed wing micro aerial vehicles. University of Notre Dame, Notre Dame, IN46556, USA, 1-32.
Related research
1. Barbarino, S.;Bilgen, O.; Friswell, M.I.;Ajai, R.M.; and Inman, D.J. (2010). A review of morphing aircraft. Journal of Intelligent Material Systems and Structures, 22(9), 823-877.
2. Friswell, M.I. (2014). Morphingaircraft: an improbable dream? Proceedings of the ASME 2014 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Newport, Rhode Island, USA,1-7. [OpenAIRE]
Vasista, S.;Tong, L.; and Wong, K.C. (2012). Realization of morphing wings: amultidisciplinary challenge. Journal of Aircraft, 49(1), 11-28.
4. Poonsong, P. (2004). Design and analysis of a multi-section variable camber wing. MSc. Thesis. University of Maryland, College Park, MD 20742, United States.
Ko, S.H.;Bae, J.S.;and Rho, J.H. (2014). Development of a morphing flap using shape memory alloy actuators: the aerodynamic characteristics of a morphing flap. Smart Materials and Structures, 23(7), 1-21.
Wang, Y. (2015). Development of flexible-rib morphing wing system. M.Sc.
Thesis. University of Toronto, 27 King's College Cir, ON M5S, Canada.
Woods, B.K.S.; Bilgen, O.; and Friswell, M.I. (2014). Wind tunnel testing of the fish bone active camber morphing concept. Journal of Intelligent Material Systems and Structures, 25(7),772-785. [OpenAIRE]
8. Counsil, J.N.N.; and Boulama, K.G. (2013). Low-Reynolds-number aerodynamic performance of NACA 0012 and Selig-Donovan 7003 airfoils. Journal of Aircraft, 50(1), 204-216.
XFLR5 ver. 6.10.04 (2014).
fromhttp://www.xflr5.com/xflr5.htm
10. Selig, M.S.; Deters, R.W.; and Williamson, G.A. (201l). Wind tunnel testing airfoils at low reynolds numbers. 49th AIAA Aerospace Sciences Meeting, Orlando, FL, 1-32.
11. Van Ingen, J.L. (2008). The eN method for transition prediction. Historical review of work at TU Delft. 38thFluid Dynamics Conference and Exhibit, Seattle, Washington, 1-49.
12. Wahidi, R.; and Bridges, D.H. (2009). Experimental investigation of the boundary layer and pressure measurements on airfoil with laminar separation bubbles. 39th AIAA Fluid Dynamics Conference, San Antonia, Texas. [OpenAIRE]
13. Muller, T.J. (1999). Aerodynamic measurements at low Reynolds numbers for fixed wing micro aerial vehicles. University of Notre Dame, Notre Dame, IN46556, USA, 1-32.