Works matching DE "AIRPLANE control surfaces"
Results: 56
Revitalising advanced rotorcraft research – and the compound helicopter.
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- Aeronautical Journal, 2016, v. 120, n. 1223, p. 83, doi. 10.1017/aer.2015.5
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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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NUMERICAL INVESTIGATION OF VISCOUS AERODYNMIC EFFECTS ON TRANSONIC FLUTTER AND LIMIT CYCLE OSCILLATIONS FOR A TYPICAL AIRFOIL.
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- International Journal of Intelligent Computing & Information Sciences, 2016, v. 16, n. 2, p. iii
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Nonlinear dynamics and stability analysis of vehicle plane motions.
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- Vehicle System Dynamics, 2007, v. 45, n. 1, p. 15, doi. 10.1080/00423110600828285
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- Article
Experimental Investigation of the Wake and the Wingtip Vortices of a UAV Model.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 4, p. 53, doi. 10.3390/aerospace4040053
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Design, Development and Testing of Shape Shifting Wing Model.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 4, p. 52, doi. 10.3390/aerospace4040052
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Active Flow Control Implemented in a Multi-Stage High-Speed Axial Compressor.
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- PAMM: Proceedings in Applied Mathematics & Mechanics, 2016, v. 16, n. 1, p. 645, doi. 10.1002/pamm.201610311
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Effect of one-sided unsteady energy supply on aerodynamic characteristics of airfoils in a transonic flow.
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- Journal of Applied Mechanics & Technical Physics, 2008, v. 49, n. 6, p. 957, doi. 10.1007/s10808-008-0118-z
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Using the perturbation method to solve the problem of separated incompressible flow past thin airfoils.
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- Journal of Applied Mechanics & Technical Physics, 2006, v. 47, n. 3, p. 346, doi. 10.1007/s10808-006-0062-8
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- Article
AIR FLOW STUDY ON THE XERVA SPACE LAUNCHER AILERON.
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- Annals of DAAAM & Proceedings, 2009, p. 527
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- Article
On the Growth of Fatigue Cracks from Material and Manufacturing Discontinuities Under Variable Amplitude Loading.
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- JOM: The Journal of The Minerals, Metals & Materials Society (TMS), 2015, v. 67, n. 6, p. 1385, doi. 10.1007/s11837-015-1437-1
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- Article
Nonlinear Control Method for Hypersonic Vehicle Based on Double Power Reaching Law of Sliding Mode.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2018, v. 35, n. 5, p. 849, doi. 10.16356/j.1005-1120.2018.05.849
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- Article
Effectiveness of Direct Current Arc Plasma Discharge on Aerodynamic Control in Hypersonic Flow.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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- Article
Design of a Stable Airfoil.
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- Doklady Physics, 2004, v. 49, n. 8, p. 471, doi. 10.1134/1.1795960
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APPLICATION OF THE 2D FINITE-ELEMENT/BOUNDARY-ELEMENT METHOD TO SCATTERING FROM COATED AEROFOILS.
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- Microwave & Optical Technology Letters, 1994, v. 7, n. 4, p. 163, doi. 10.1002/mop.4650070402
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- Article
Design and analysis of lateral motion control algorithms for an unmanned aerial vehicle with two control surfaces.
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- Automation & Remote Control, 2017, v. 78, n. 5, p. 924, doi. 10.1134/S0005117917050137
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- Article
Effect of Strakes on the Aerodynamic Performance of a One-Half Power-Law Body with Elliptical Cross-Section.
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- International Review of Aerospace Engineering, 2011, v. 4, n. 1, p. 29
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Analytical Redundancy in Torque Summed Multi-Lane Smart Electromechanical Actuators.
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- International Review of Aerospace Engineering, 2011, v. 4, n. 1, p. 20
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- Article
INVERSE DESIGN OF 2-D AIRFOIL VIA VIBRATIONAL GENETIC ALGORITHM.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2006, v. 2, n. 4, p. 7
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- Article
SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2006, v. 2, n. 4, p. 1
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- Article
Calculation and Identification of the Aerodynamic Parameters for Small-Scaled Fixed-Wing UAVs.
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- Sensors (14248220), 2018, v. 18, n. 1, p. 206, doi. 10.3390/s18010206
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Analysis of the Effects of Thermal Environment on Optical Systems for Navigation Guidance and Control in Supersonic Aircraft Based on Empirical Equations.
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- Sensors (14248220), 2016, v. 16, n. 10, p. 1717, doi. 10.3390/s16101717
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Nonuniqueness of the Transonic Flow past an Airfoil.
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- Fluid Dynamics, 2004, v. 39, n. 4, p. 642, doi. 10.1023/B:FLUI.0000045680.74521.80
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- Article
Analytic Solution in the Problem of Constructing an Airfoil with Minimum Wave Drag.
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- Fluid Dynamics, 2003, v. 38, n. 6, p. 933, doi. 10.1023/B:FLUI.0000015235.61628.78
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- Article
Aerodynamic Performance Investigation of an Experimental Variable-Span Morphing Wing Model.
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- Journal of Applied & Computational Sciences in Mechanics, 2016, v. 27, n. 1, p. 201
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- Article
Model checking aircraft controller software: a case study.
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- Software: Practice & Experience, 2015, v. 45, n. 7, p. 989, doi. 10.1002/spe.2242
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Changes of growth characteristics and free amino acid content of cultivated Porphyra yezoensis Ueda (Bangiales Rhodophyta) blades with the progression of the number of harvests in a nori farm.
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- Journal of Applied Phycology, 2008, v. 20, n. 5, p. 687, doi. 10.1007/s10811-007-9273-5
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- Article
An Effective Algorithm of Aerodynamic Control over Spacecraft Descent.
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- Cosmic Research, 2005, v. 43, n. 6, p. 450, doi. 10.1007/s10604-005-0069-6
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- Article
Optimization of Transmission Mechanism with Cable Networks for Morphing Trailing-Edge.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 2, p. 292
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- Article
Guidance, navigation and control of a powered parafoil aerial vehicle.
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- Current Science (00113891), 2016, v. 111, n. 6, p. 1045, doi. 10.18520/cs/v111/i6/1045-1054
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- Article
Numerical investigation of aeroheating characteristics of spiked blunt bodies at Mach six flight conditions.
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- Aeronautical Journal, 2011, v. 115, n. 1168, p. 377, doi. 10.1017/S0001924000005893
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- Article
Modification impact on aerodynamic performance of hypersonic waverider.
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- Aeronautical Journal, 2011, v. 115, n. 1168, p. 325, doi. 10.1017/S0001924000005844
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- Article
Subsonic aerofoil design 2010.
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- Aeronautical Journal, 2011, v. 115, n. 1165, p. 137, doi. 10.1017/S0001924000005546
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Identification of a MIMO state space model of an F/A-18 aircraft using a subspace method.
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- Aeronautical Journal, 2009, v. 113, n. 1141, p. 183, doi. 10.1017/S0001924000700418
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- Article
A circulation control actuator for flapless flight control.
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- Aeronautical Journal, 2008, v. 112, n. 1134, p. 483, doi. 10.1017/S0001924000002451
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- Article
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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- Article
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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- Article
Flow control with active dimples.
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- Aeronautical Journal, 2007, v. 111, n. 1125, p. 705, doi. 10.1017/S0001924000004887
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- Article
The longitudinal flying qualities of a blended-wing-body civil transport aircraft.
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- Aeronautical Journal, 2004, v. 108, n. 1080, p. 75, doi. 10.1017/S0001924000005029
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- Article
An investigation into the longitudinal dynamics and control of a flapping wing micro air vehicle at hovering flight.
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- Aeronautical Journal, 2003, v. 107, n. 1078, p. 743, doi. 10.1017/s0001924000013506
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- Article
The effects of apex flap on the leading-edge vortex breakdown of a cropped double delta wing.
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- Aeronautical Journal, 2003, v. 107, n. 1078, p. 739, doi. 10.1017/s000192400001349x
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Design of a turbulent wing for small aircraft using multidisciplinary optimisation.
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- Archives of Mechanics, 2014, v. 66, n. 3, p. 185
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- Article
THE AERODYNAMIC ANALYSIS OF HIGH LIFT DEVICES.
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- Scientific Research & Education in the Air Force - AFASES, 2014, v. 1, p. 83
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- Article
THE DRIVELINE ANALYSIS OF HYPER SUSTENTATION DEVICES.
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- Scientific Research & Education in the Air Force - AFASES, 2014, v. 1, p. 61
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- Article
Simple adaptive bank-reversal control for non-linear winged re-entry vehicles.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2018, v. 9, n. 1, p. 85
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- Article
SlidingMode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle.
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- International Journal of Aerospace Engineering, 2010, p. 1, doi. 10.1155/2010/474537
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- Article
LES prediction of wall-pressure fluctuations and noise of a low-speed airfoil.
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- International Journal of Aeroacoustics, 2009, v. 8, n. 3, p. 177, doi. 10.1260/147547208786940017
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- Article
A Numerical Model to Study the Nonlinear and Unsteady Aerodynamics of Bioinspired Morphing-Wing Concepts.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 327, doi. 10.1260/1756-8293.7.3.327
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- Article
Experimental and Numerical Studies on Aerodynamic Control of NACA 4418 Airfoil with a Rotating Cylinder.
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- Journal of Vibration Engineering & Technologies, 2020, v. 8, n. 1, p. 141, doi. 10.1007/s42417-019-00085-5
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- Article
Design concepts of an aircraft wing: composite and morphing airfoil with auxetic structures.
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- Frontiers of Structural & Civil Engineering, 2016, v. 10, n. 4, p. 394, doi. 10.1007/s11709-016-0352-z
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- Article