000			06442cam a22004574i 4500
005			20211105144036.0
008			020613s2002 gw a b 100 0 eng d
010			_a 2002283437
011			_aChanged OCLC from 49286489 to 50859224
020			_a3540426965 _qhd.bd.
020			_a9783540426967 _qhd.bd.
035			_a(ATU)b10259661
035			_a(DLC) 2002283437
035			_a(OCoLC)50859224
040			_aDLC _beng _erda _dATU
042			_alccopycat
050	0	0	_aTL570. _bA493 2000
082	0		_a629.1323
111	2		_aAG STAB/DGLR Symposium _n(12th : _d2000 : _cStuttgart, Germany)
245	1	0	_aNew results in numerical and experimental fluid mechanics III : _bcontributions to the 12th STAB/DGLR symposium, Stuttgart, Germany, 2000 / _cSiegfried Wagner [and others] (editors).
264		1	_aBerlin ; _aNew York : _bSpringer, _c[2002]
264		4	_c©2002
300			_axii, 433 pages : _billustrations (some colour) ; _c24 cm.
336			_atext _btxt _2rdacontent
337			_aunmediated _bn _2rdamedia
338			_avolume _bnc _2rdacarrier
490	1		_aNotes on numerical fluid mechanics, _x0179-9614 ; _vv. 77
504			_aIncludes bibliographical references.
505	0	0	_tDesign Work for the A3XX High-Lift-Wing -- _tRecent Improvements in the Measurement of Aerodynamic Damping Derivatives -- _tCalculation of Horizontal Stabilizer Efficiency with a Navier-Stokes Code -- _t3D RANS Simulations for High-Lift Analysis of Transport Aircraft Configurations -- _tNumerical Investigation of the Reynolds-Number-Effect on the Setting Sensitivity of a 2D High-Lift Multi-Element Airfoil -- _tSeparation Control on a High-Lift Configuration by Periodic Exitation -- _tNumerical Investigation of the Effect of the High-Lift Configuration of a Transport Aircraft on its Vortex Wake -- _tThe Relationship Between Near- and Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings -- _tInfluence of Different Flap Settings on the Hazard Posed to Following Aircraft -- _tNumerical Simulation of Wake-Vortex Encounters Using the Chimera-Technique -- _tAspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation -- _tCoupling of DLR Navier-Stokes Solver FLOWer with an e[superscript N]-Database Method for Laminar-Turbulent Transition Prediction on Airfoils -- _tUnsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Gottingen (DNW-TWG) -- _tTurbulence Modeling for Reentry-Vehicles -- _tComputation of the Two-Dimensional Flow in SERN Nozzles -- _tExperimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC -- _tAerodynamic Analysis of the Dual-Mode Ramjet Vehicle JAPHAR -- _tStudy of Shock-Wave/Boundary-Layer Interaction Flowfield on a 24[superscript [degree]] Ramp Model -- _tNumerical Investigations of Small-Amplitude Disturbances in a Laminar Boundary Layer with Impinging Shock Waves -- _tSurface Temperature Effects on Shock-Wave Boundary-Layer Interaction of Ramp Flows -- _tPreliminary Results of Numerical Simulations of Elastic Panels in Transonic Flows -- _tNumerical Simulation of Laminar Separation-Bubble Control -- _tOn the Structure of Turbulence in the Transition Cylinder Wake -- _tInvestigation of Subgrid-Scale Models in LES of Turbulent Flows with Separation -- _tExperimental and Numerical Investigations on Transition in a Laminar Separation Bubble -- _tBoundary-layer Separation Computed by Second-Moment Closure Models -- _tExperimental Investigation on the Behaviour of Disturbances Emitted from a Point Source in a Laminar Boundary Layer -- _tExperimental/Numerical Investigation of the Influence of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of an Airfoil -- _tInterference of Wave Trains with Varying Phase Relations in a Decelerated Two-Dimensional Boundary Layer -- _tSecondary Instability of Steady and Unsteady Crossflow Waves -- _tExamination of the Eddy-Viscosity Concept Regarding its Physical Justification -- _tA Numerical Method for Compressible and Low Mach Number Fluid Flow -- _tTurbulent Two-Dimensional Flow Around a Flexible Membrane Airfoil -- _tSolution of the Euler Equations on Locally Adaptive B-Spline Grids -- _tAn Algorithm to Treat Flows Bounded by Arbitrarity Shaped Surfaces with Cartesian Meshes -- _tGrid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI -- _tConvergence Acceleration on Unstructured Meshes -- _tEnhancement of a Navier-Stokes Flow Solver for Patched Grids with Non-Coincident Grid Nodes -- _tFlow and Turbulence Structures in the Wake of a Simplified Car Model (Ahmed Modell) -- _tFlow Visualisation, Pressure Measurements and Numerical Calculations on Spike-Tipped Bodies -- _tTip-Vortices in Transonic Axial-Compressors -- _tAirframe Noise - Generation and Reduction - a Report on Status and Perspectives of DLR-Research -- _tReceptivity of Three-Dimensional Boundary Layers to Roughness and Suction - Linear and Nonlinear Effects -- _tActive Control of Tollmien-Schlichting Instabilities by Multi-Channel Sensor Actuator Systems -- _tTime Resolved 2D Measurement Techniques for Quantitative Determination of Flow Fields and Surface Pressure Distributions -- _tInvestigation of Transitional Structures in Artificially and Disturbed Excited Flat Plate Boundary Layer Flows Using Stereo and Multi-Plane PIV -- _tThe Meaning of Disturbance Fields in Transition Experiments and Their Detection in the Test Section Flow of a Short Duration Wind Tunnel -- _tSurface Fence with an Integrated, Piezoresistive Pressure Sensor for Measurements of Static and Dynamic Wall Shear Stress -- _tExperimental Investigation of the Flow Close to the Surface of a High Lift Airfoil Configuration in a Large Wind Tunnel -- _tDetection of Density Gradients at Helicopter Rotor Blades in Flight.
588			_aMachine converted from AACR2 source record.
650		0	_aAerodynamics _vCongresses _9693834
650		0	_aAirplanes _xDesign and construction _vCongresses _9786228
650		0	_aFluid dynamics _vCongresses _9690211
650		0	_aTurbulence _vCongresses _9693839
700	1		_aWagner, Siegfried, _cDr. Ing.
830		0	_aNotes on numerical fluid mechanics ; _vv. 77. _9233862
907			_a.b10259661 _b09-11-17 _c27-10-15
998			_ab _ac _b06-04-16 _cm _da _feng _ggw _h0
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