Works matching DE "FLUID dynamics"
Results: 5000
Of other seas: metaphors and materialities in maritime regions.
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- Atlantic Studies, 2013, v. 10, n. 2, p. 156, doi. 10.1080/14788810.2013.785192
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- Article
Enhanced flow visualisation of complex aerodynamic phenomena using automatic stream surface seeding with application to the BLOODHOUND SSC Land Speed Record vehicle.
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- Aeronautical Journal, 2016, v. 120, n. 1226, p. 547, doi. 10.1017/aer.2016.10
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Unified approach for conjugate heat-transfer analysis of high speed air flow through a water-cooled nozzle.
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- Aeronautical Journal, 2016, v. 120, n. 1224, p. 355, doi. 10.1017/aer.2015.15
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AER volume 120 issue 1223 Cover and Front matter.
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- Aeronautical Journal, 2016, v. 120, n. 1223, p. f1, doi. 10.1017/aer.2016.2
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- Article
Understanding of flow features over a typical crew module at Mach 4.
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- Aeronautical Journal, 2015, v. 119, n. 1216, p. 727, doi. 10.1017/S0001924000010794
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Numerical validation and back-pressure effect on internal compression flows of typical supersonic inlet.
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- Aeronautical Journal, 2015, v. 119, n. 1215, p. 631, doi. 10.1017/S0001924000010721
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Numerical investigation of secondary flows in a constant-width wind-tunnel contraction.
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- Aeronautical Journal, 2015, v. 119, n. 1215, p. 613, doi. 10.1017/S000192400001071X
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Experimental investigation of the rotor-wing aerodynamic interaction in a tiltwing aircraft in hover.
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- Aeronautical Journal, 2015, v. 119, n. 1215, p. 591, doi. 10.1017/S0001924000010708
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Introduction to Compressible Fluid Flow - Second edition.
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- 2014
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- Book Review
Aerothermodynamics of a hypersonic projectile with a double-disk aerospike.
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- Aeronautical Journal, 2013, v. 117, n. 1195, p. 913, doi. 10.1017/S0001924000008587
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High resolution computation of compressible condensing/evaporating moist-air flow for external and internal flows.
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- Aeronautical Journal, 2013, v. 117, n. 1190, p. 427, doi. 10.1017/S0001924000008083
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Rapid, parallel CFD grid generation using octrees.
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- Aeronautical Journal, 2013, v. 117, n. 1188, p. 133, doi. 10.1017/S0001924000007910
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Numerical investigation of optimal pin location on a supersonic projectile.
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- Aeronautical Journal, 2012, v. 116, n. 1177, p. 271, doi. 10.1017/S0001924000006837
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Influence of stores on the flow inside UCAV weapon bays.
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- Aeronautical Journal, 2012, v. 116, n. 1176, p. 199, doi. 10.1017/S0001924000006709
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- Article
Computational investigation of cavity flow control using a passive device.
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- Aeronautical Journal, 2012, v. 116, n. 1176, p. 153, doi. 10.1017/S0001924000006679
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Flexible flapping systems: computational investigations into fluid-structure interactions.
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- Aeronautical Journal, 2011, v. 115, n. 1172, p. 593, doi. 10.1017/S000192400000628X
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Study of jets from rectangular nozzles with square grooves.
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- Aeronautical Journal, 2011, v. 115, n. 1165, p. 187, doi. 10.1017/S0001924000005583
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Effects of boundary-layer bleeding on unstart oscillatory flow of hypersonic inlets.
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- Aeronautical Journal, 2010, v. 114, n. 1157, p. 445, doi. 10.1017/S0001924000003924
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Flow visualisation of the helicopter brown-out phenomenon.
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- Aeronautical Journal, 2009, v. 113, n. 1145, p. 467, doi. 10.1017/S0001924000003134
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A calculation method for parametric design studies of V/STOL aircraft.
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- Aeronautical Journal, 2009, v. 113, n. 1143, p. 309, doi. 10.1017/S0001924000002980
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- Article
Downward pointing winglet design and assessment within the M-DAW research project.
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- Aeronautical Journal, 2009, v. 113, n. 1142, p. 221, doi. 10.1017/S000192400000289X
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Predicting the response of low-aspect ratio, flexible aircraft.
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- Aeronautical Journal, 2009, v. 113, n. 1142, p. 207, doi. 10.1017/S0001924000002888
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Numerical simulation of fluid-structure interaction in the opening process of conical parachute.
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- Aeronautical Journal, 2009, v. 113, n. 1141, p. 191, doi. 10.1017/S0001924000011477
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Numerical and experimental investigation of tip leakage flow and heat transfer using idealised rotor-tip models at transonic conditions.
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- Aeronautical Journal, 2009, v. 113, n. 1141, p. 165, doi. 10.1017/S0001924000011453
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- Article
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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- Article
Comparison between blade-element models of propellers.
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- Aeronautical Journal, 2008, v. 112, n. 1138, p. 689, doi. 10.1017/S0001924000002669
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Performance simulation of a high-bypass turbofan with a 2D representation of the intake and fan components.
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- Aeronautical Journal, 2008, v. 112, n. 1137, p. 673, doi. 10.1017/S0001924000002645
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Cold flow analysis of trapped vortex combustor using two equation turbulence models.
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- Aeronautical Journal, 2008, v. 112, n. 1136, p. 569, doi. 10.1017/S0001924000002530
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A low-Reynolds-number one-equation model of turbulence.
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- Aeronautical Journal, 2008, v. 112, n. 1128, p. 101, doi. 10.1017/S0001924000002037
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Method for aerodynamic unsteady forces time calculations on an F/A-18 aircraft.
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- Aeronautical Journal, 2008, v. 112, n. 1127, p. 27, doi. 10.1017/S0001924000001962
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Induced drag and wake kinetic energy.
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- Aeronautical Journal, 2008, v. 112, n. 1127, p. 54, doi. 10.1017/S0001924000087753
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Experimental and computational investigation into the use of co-flow fluidic thrust vectoring on a small gas turbine.
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- Aeronautical Journal, 2008, v. 112, n. 1127, p. 17, doi. 10.1017/S0001924000001950
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Modelling the interaction of helicopter main rotor and tail rotor wakes.
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- Aeronautical Journal, 2007, v. 111, n. 1124, p. 637, doi. 10.1017/S0001924000004814
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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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Achieving high parallel performance for an unstructured unsteady turbomachinery CFD code.
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- Aeronautical Journal, 2007, v. 111, n. 1117, p. 185, doi. 10.1017/S0001924000004449
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- Article
An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion control analysis.
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- Aeronautical Journal, 2007, v. 111, n. 1117, p. 133, doi. 10.1017/S0001924000004395
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3D numerical simulation of the supersonic combustion of H<sub>2</sub>.
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- Aeronautical Journal, 2006, v. 110, n. 1114, p. 773, doi. 10.1017/S0001924000001640
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Some hypersonic intake studies.
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- Aeronautical Journal, 2006, v. 110, n. 1105, p. 145, doi. 10.1017/S0001924000001123
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- Article
Introduction to Computational Fluid Dynamics.
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- 2006
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- Book Review
Comparison of a grid-based CFD method and vortex dynamics predictions of low Reynolds number cylinder flows.
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- Aeronautical Journal, 2006, v. 110, n. 1103, p. 63
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A feasiblity study on designing model support systems for a blended wing body configuration in a transonic wind tunnel.
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- Aeronautical Journal, 2006, v. 110, n. 1103, p. 53
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- Article
CFD fire simulation of the Swissair flight 111 in-flight fire - Part 1: Prediction of the pre-fire air flow within the cockpit and surrounding areas.
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- Aeronautical Journal, 2006, v. 110, n. 1103, p. 41, doi. 10.1017/S0001924000004358
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- Article
Status and perspectives of laminar flow.
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- Aeronautical Journal, 2005, v. 109, n. 1102, p. 639, doi. 10.1017/S000192400000097X
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A review of recent developments in flow control.
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- Aeronautical Journal, 2005, v. 109, n. 1095, p. 205, doi. 10.1017/S0001924000005200
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- Article
A theoretical description of viscous flow along a flat plate.
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- Aeronautical Journal, 2005, v. 109, n. 1101, p. 585, doi. 10.1017/S0001924000000920
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- Article
Application of Java and VRML visualisation tools in store release wind-tunnel testing.
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- Aeronautical Journal, 2005, v. 109, n. 1101, p. 569
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- Article
PIV measurements in a twin-jet STOVL fountain flow.
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- Aeronautical Journal, 2005, v. 109, n. 1100, p. 439, doi. 10.1017/S0001924000000853
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- Article
Normal shock wave/turbulent boundary-layer interaction control using ‘smart’ piezoelectric actuators.
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- Aeronautical Journal, 2005, v. 109, n. 1101, p. 577, doi. 10.1017/S0001924000000919
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- Article
The behaviour of circular synthetic jets in a laminar boundary layer.
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- Aeronautical Journal, 2005, v. 109, n. 1100, p. 461, doi. 10.1017/S0001924000000877
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- Article
Shock-wave induced instability in internal explosion dynamics.
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- Aeronautical Journal, 2005, v. 109, n. 1101, p. 537, doi. 10.1017/S0001924000000890
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- Article