Works matching DE "AEROFOILS"
Results: 1899
Experimental investigation of flowfield over an iced aerofoil.
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- Aeronautical Journal, 2016, v. 120, n. 1227, p. 735, doi. 10.1017/aer.2016.29
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Simplified propeller analysis and design including effects of stall.
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- Aeronautical Journal, 2016, v. 120, n. 1227, p. 796, doi. 10.1017/aer.2016.31
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Drag optimisation of a wing equipped with a morphing upper surface.
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- Aeronautical Journal, 2016, v. 120, n. 1225, p. 473, doi. 10.1017/aer.2016.6
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DLR natural and hybrid transonic laminar wing design incorporating new methodologies.
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- Aeronautical Journal, 2015, v. 119, n. 1221, p. 1303, doi. 10.1017/S0001924000011283
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Repetitively enhanced neural networks method for complex engineering design optimisation problems.
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- Aeronautical Journal, 2015, v. 119, n. 1220, p. 1253, doi. 10.1017/S0001924000011234
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Estimating aerofoil lift from flow angle.
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- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1167, doi. 10.1017/S0001924000011180
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A technique to predict the aerodynamic effects of battle damage on an aircraft's wing.
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- Aeronautical Journal, 2015, v. 119, n. 1218, p. 937, doi. 10.1017/S0001924000004267
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Optimum design of a PID controller for the adaptive torsion wing.
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- Aeronautical Journal, 2015, v. 119, n. 1217, p. 871, doi. 10.1017/S0001924000010964
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Effects of surface flow visualisation on aerodynamic loads at low Reynolds number.
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- Aeronautical Journal, 2015, v. 119, n. 1215, p. 663, doi. 10.1017/S0001924000010745
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The effect of the aerofoil thickness on the performance of the MAV scale cycloidal rotor.
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- Aeronautical Journal, 2015, v. 119, n. 1213, p. 343, doi. 10.1017/S0001924000010502
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Vibration analyses of an equivalent plate wing with an external store.
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- Aeronautical Journal, 2014, v. 118, n. 1207, p. 1090, doi. 10.1017/S0001924000009763
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Aerodynamic study of aerofoil and wing in simulated rain environment via a two-way coupled Eulerian-Lagrangian approach.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 643, doi. 10.1017/S0001924000009416
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Transonic aerofoils admitting anomalous behaviour of lift coefficient.
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- Aeronautical Journal, 2014, v. 118, n. 1202, p. 425, doi. 10.1017/S0001924000009209
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Aerodynamic performance benefits of utilising camber morphing wings for unmanned air vehicles.
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- Aeronautical Journal, 2013, v. 117, n. 1189, p. 315, doi. 10.1017/S0001924000008010
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The estimation of aerodynamic forces on flat plate aerofoils at hypersonic and supersonic speed.
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- Aeronautical Journal, 2012, v. 116, n. 1185, p. 1207, doi. 10.1017/S0001924000007570
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Investigation of skin porosity damping effects on free stream disturbance induced unsteady wing loads.
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- Aeronautical Journal, 2012, v. 116, n. 1184, p. 1041, doi. 10.1017/S0001924000007478
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Aerodynamic and performance characteristics of a passive leading edge Kruger flap at low Reynolds numbers.
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- Aeronautical Journal, 2012, v. 116, n. 1181, p. 757, doi. 10.1017/S0001924000007211
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Aerodynamics of an aerofoil in transonic ground effect: Methods for blowdown wind-tunnel scale testing.
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- Aeronautical Journal, 2012, v. 116, n. 1180, p. 599, doi. 10.1017/S0001924000007090
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Aerodynamics of an aerofoil in transonic ground effect: numerical study at full-scale Reynolds numbers.
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- Aeronautical Journal, 2012, v. 116, n. 1178, p. 407, doi. 10.1017/S0001924000005297
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Use of aerofoil section dynamic stall synthesis methods in rotor design.
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- Aeronautical Journal, 2012, v. 116, n. 1179, p. 501, doi. 10.1017/S0001924000007004
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Advancement of aerofoil section dynamic stall synthesis methods for rotor design.
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- Aeronautical Journal, 2012, v. 116, n. 1179, p. 521, doi. 10.1017/S0001924000007016
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Analysis of compressible potential flow over aerofoils using the dual reciprocity method.
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- Aeronautical Journal, 2012, v. 116, n. 1178, p. 391, doi. 10.1017/S0001924000005285
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Parametric studies of aerofoil-vortex interaction; a numerical approach using LES.
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- Aeronautical Journal, 2011, v. 115, n. 1173, p. 703, doi. 10.1017/S0001924000006424
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Trailing-edge flap flow control for dynamic stall.
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- Aeronautical Journal, 2011, v. 115, n. 1170, p. 493, doi. 10.1017/S0001924000006138
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Aerofoil flow separation suppression using dimples.
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- Aeronautical Journal, 2011, v. 115, n. 1168, p. 335, doi. 10.1017/S0001924000005856
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The influence of Reynolds and Mach numbers on two-dimensional wind-tunnel testing: An experience.
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- Aeronautical Journal, 2011, v. 115, n. 1166, p. 249, doi. 10.1017/S0001924000005704
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Dynamics of the wing-tip vortex in the near field of a NACA 0012 aerofoil.
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- Aeronautical Journal, 2011, v. 115, n. 1166, p. 229, doi. 10.1017/S0001924000005686
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Development and validation of an efficient direct numerical optimisation approach for aerofoil shape design.
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- Aeronautical Journal, 2010, v. 114, n. 1160, p. 611, doi. 10.1017/S0001924000004097
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Flutter control using resistively shunted piezoceramics.
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- Aeronautical Journal, 2010, v. 114, n. 1156, p. 387, doi. 10.1017/S0001924000003845
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Aerodynamic study of corrugated skins for morphing wing applications.
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- Aeronautical Journal, 2010, v. 114, n. 1154, p. 237, doi. 10.1017/S0001924000003687
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Validation study for prediction of iced aerofoil aerodynamics.
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- Aeronautical Journal, 2010, v. 114, n. 1152, p. 103, doi. 10.1017/S0001924000003572
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Flutter/LCO suppression for high-aspect ratio wings.
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- Aeronautical Journal, 2009, v. 113, n. 1144, p. 409, doi. 10.1017/S0001924000003079
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Macro-fiber composite actuators for a swept wing unmanned aircraft.
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- Aeronautical Journal, 2009, v. 113, n. 1144, p. 385, doi. 10.1017/S0001924000003055
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Pneumatic flow control studies using steady blowing on a supercritical aerofoil.
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- Aeronautical Journal, 2009, v. 113, n. 1139, p. 53, doi. 10.1017/S0001924000002773
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Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil.
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- Aeronautical Journal, 2008, v. 112, n. 1138, p. 705, doi. 10.1017/S0001924000002670
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Transitional separation bubbles and unsteady aspects of aerofoil stall.
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- Aeronautical Journal, 2008, v. 112, n. 1133, p. 395, doi. 10.1017/S0001924000002359
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Numerical simulation of rime ice accretions on an aerofoil using an Eulerian method.
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- Aeronautical Journal, 2008, v. 112, n. 1131, p. 243, doi. 10.1017/S0001924000002189
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Periodic transonic flow and control.
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- Aeronautical Journal, 2008, v. 112, n. 1127, p. 1, doi. 10.1017/S0001924000001949
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The onset of compressibility effects for aerofoils in ground effect.
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- Aeronautical Journal, 2007, v. 111, n. 1126, p. 797, doi. 10.1017/S0001924000001913
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Effect of plunging amplitude on the performance of a wind turbine blade section.
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- Aeronautical Journal, 2007, v. 111, n. 1123, p. 571, doi. 10.1017/S0001924000001846
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Measuring the effect of helicopter rotors on GPS reception.
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- Aeronautical Journal, 2007, v. 111, n. 1123, p. 561, doi. 10.1017/S0001924000001834
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Computational and experimental investigations of low-Reynolds-number flows past an aerofoil.
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- Aeronautical Journal, 2007, v. 111, n. 1115, p. 17, doi. 10.1017/S000192400000172X
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Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method.
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- Aeronautical Journal, 2006, v. 110, n. 1111, p. 589, doi. 10.1017/S0001924000001457
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Aerodynamic effectiveness of the flow of exhaust gases in a generic formula one car configuration.
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- Aeronautical Journal, 2006, v. 110, n. 1111, p. 573, doi. 10.1017/S0001924000001445
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Bio-inspired design of flapping-wing micro air vehicles.
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- Aeronautical Journal, 2005, v. 109, n. 1098, p. 385, doi. 10.1017/S0001924000000804
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Control of trailing-edge separation by tangential blowing inside the bubble.
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- Aeronautical Journal, 2004, v. 108, n. 1086, p. 419, doi. 10.1017/S0001924000000233
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Aeroelastically adaptive propeller using blades' root flexibility.
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- Aeronautical Journal, 2004, v. 108, n. 1086, p. 411, doi. 10.1017/S0001924000000221
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Closed-loop flutter control using strain actuation.
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- Aeronautical Journal, 2004, v. 108, n. 1083, p. 271, doi. 10.1017/S0001924000005133
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Oscillating behaviour of laminar separation bubble formed on an aerofoil near stall.
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- Aeronautical Journal, 2004, v. 108, n. 1081, p. 153, doi. 10.1017/S0001924000151607
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Experimental investigation on wall pressure distribution in flaps' separating regions.
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- Aeronautical Journal, 2004, v. 108, n. 1080, p. 103, doi. 10.1017/S0001924000005054
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