PORTO-
FREI

New Results in Numerical and Experimental Fluid Mechanics V

Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004

This volume collects contributions to the 14th Symposium of the STAB (German Aerospace Aerodynamics Association). The association involves German scientists and engineers from universities, research establishments and industry who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but for other applications, too. The volume gives a broad overview of ongoing work in Germany in this field.

Buch (Gebunden)

EUR 320,99

Alle Preisangaben inkl. MwSt.

Auch verfügbar als:

  Verlagsbedingte Lieferzeit ca. 3 - 6 Werktage.
(Print on Demand. Lieferbar innerhalb von 3 bis 6 Tagen)

Versandkostenfrei*

Dieser Artikel kann nicht bestellt werden.
 

Produktbeschreibung

This volume collects contributions to the 14th Symposium of the STAB (German Aerospace Aerodynamics Association). The association involves German scientists and engineers from universities, research establishments and industry who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but for other applications, too. The volume gives a broad overview of ongoing work in Germany in this field. 

Inhaltsverzeichnis

High Aspect-Ratio Wings.- High Reynolds-Number Windtunnel Testing for the Design
of Airbus High-Lift Wings.- Aerodynamic Analysis of Flows with Low Mach- and
Reynolds-Number under Consideration and Forecast of Transition on the Example of
a Glider.- Analysis of PIV Flow Measurements behind the ALVAST-Model in
High-Lift Configuration.- Effect of Differential Flap Settings on the Wake
Vortex Evolution of Large Transport Aircraft.- Investigations on the Influence
of Fins on the Extended Nearfield of a Wing inHigh-Lift Configuration.-
Application of the PSP Technique in Low Speed Wind Tunnels.- Investigation of
tailplane stall for a generic transport aircraft configuration.- Numerical
analysis of transport aircraft using different wing tip devices.- Aerodynamic
Optimisation of a Flying Wing Transport Aircraft.- Low Aspect-Ratio Wings.-
Delta Wing Steady Pressure Investigations for Sharp and Rounded Leading Edges.-
Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged
Navier-Stokes Solver.- Experimental study on the Flowfield of a
Delta-Canard-Configuration with Deflected Leading Edge.- Numerical simulation of
maneuvering combat aircraft.- Experimental investigation on periodic rolling of
a delta wing flow at transonic Mach numbers.- Numerical Design of a Low-Noise
High-Lift System for a Supersonic Aircraft.- Helicopters.- Chimera Simulation of
a Complete Helicopter with Rotors as Actuator Discs.- Extension of the
Unstructured TAU-Code for Rotating Flows.- Unsteady Euler and Navier-Stokes
Simulations of Propellers with the Unstructured DLR TAU-Code.- Aerodynamic
Analysis of Jet-Blast using CFD considering as example a Hangar and an AIRBUS
A380 configuration.- Bluff Bodies.- Flow Field Study of a Supersonic Jet Exiting
into a Supersonic Stream.- Behavior of Supersonic Overexpanded Jets Impinging on
Plates.- Study of Supersonic Flow Separation Induced by a Side Jet and its
Control.- Analytically obtained data compared with shock tunnel heat flux
measurements at a conical body at M = 6.- Laminar Flow Control and Transition.-
Navier-Stokes Airfoil Computations with Automatic Transition Prediction using
the DLR TAU Code - A Sensitivity Study.- Prediction of attachment line
transition for a high-lift wing based on two-dimensional flow calculations with
RANS-solver.- RANS Simulation and Experiments on the Stall Behaviour of a
Tailplane Airfoil.- Experimental and Numerical Investigations of Flow Separation
and Transition to Turbulence in an Axisymmetric Diffuser.- In-Flight and Wind
Tunnel Investigalions of Instabilities on a Laminar Wing Glove.- Steady
three-dimensional Streaks and their Optimal Growth in a Laminar Separation
Bubble.- Applicability and quality of linear stability theory and linear PSE in
swept laminar separation bubbles.- Active Flow Control.- Drag Reduction of an
Ahmed Car Model by Means of Active Separation Control at the Rear Vehicle
Slant.- Increasing Lift by Means of Active Flow Control on the Flap of a Generic
High-Lift Configuration.- Influencing the Mixing Process in a Turbulent Boundary
Layer by Pulsed Jet Actuators.- Active Flow Control by Surface Smooth Plasma
Actuators.- Hypersonic Flows.- Boundary Layer Influence on Supersonic
Jet/Cross-Flow Interaction in Hypersonic Flow.- Numerical Rebuilding of a
Generic Body-Flap Model in an Arc Heated Facility.- Experimental and Numerical
Investigations of Shock/Turbulent Boundary Layer Interaction on a Double Ramp
Configuration.- Time Accurate Simulation of Turbulent Nozzle Flow by the DLR
TAU-Code.- Quantitative Comparison of Measured and Numerically Simulated Erosion
Rates of SiC Based Heat Shield Materials.- High-End Concept to Launch
Micro-Satellites into Low-Earth-Orbit based on Combination of a Two-Stage Rocket
and a Railgun-System.- Aeroelasticity.- Numerical Simulation of Steady and
Unsteady Aerodynamics of the WIONA (Wing with Oscillating Nacelle)
Configuration.- Computation of the Flutter Boundary of the NLR 7301 Airfoil in
the Transonic Range.- Aeroacoustics.- The Noise Criteria within
Multidisciplinary High-Lift Design.- Effect of Noise Reducing Modifications of
the Slat on Aerodynamic Properties of the High-Lift System.- Experimental Study
on Noise Reduction through Trailing Edge Brushes.- A Study on Trailing Edge
Noise Sources Using High~Speed Particle Image Velocimetry.- Towards the
Applicability of the Modified von Kßrmßn Spectrum to Predict Trailing Edge
Noise.- Numerical simulation of combustion noise using acoustic perturbation
equations.- Mathematical Fundamentals/Numerical Simulation.- Toward efficient
solution of the compressible Navier-Stokes equations.- Direct Numerical
Simulation of a Turbulent Flow Using a Spectral/hp Element Method.- Numerical
simulation of aerodynamic problems with a Reynolds stress turbulence model.-
Efficient Large-Eddy Simulation of Low Mach Number Flow.- Implementation and
Usage of Structured Algorithms within an Unstructured CFD-Code.- Numerical Flow
Simulation with Moving Grids.- Appropriate Turbulence Modelling for
Turbomachinery Flows using a Two-Equation Turbulence Model.- Numerical
determination of dynamic derivatives for transport aircraft.- Detached-eddy
simulation of the delta wing of a generic aircraft configuration.- Small
Disturbance Navier-Stokes Equations: Application on Transonic Two-dimensional
Flows Around Airfoils.- Numerical and experimental investigations of turbulent
convection with separation in aircraft cabins.- Physical Fundamentals.-
Investigation of Influence of Different Modelling Parameters on Calculation of
Transonic Buffet Phenomena.- Anisotropy Evolution in Relaminarizing Turbulent
Boundary Layers: a DNS-aided Second-Moment Closure Analysis.- Turbulent Channel
Flow with Periodic Hill Constrictions.- Turbulent Flow Separation Control by
Boundary-Layer Forcing: A Computational Study.- Facilities.- Implementation of
Propeller Simulation Techniques at DNW. 

Mehr vom Verlag:

k.A.

Produktdetails

Medium: Buch
Format: Gebunden
Seiten: 548
Sprache: Englisch
Erschienen: August 2006
Auflage: 2006
Maße: 241 x 160 mm
Gewicht: 980 g
ISBN-10: 3540332863
ISBN-13: 9783540332862
Verlagsbestell-Nr.: 11732532

Bestell-Nr.: 5042640 
Libri-Verkaufsrang (LVR):
Libri-Relevanz: 0 (max 9.999)
Bestell-Nr. Verlag: 11732532

LIBRI: 0000000
LIBRI-EK*: 230.99 € (23.00%)
LIBRI-VK: 320,99 €
Libri-STOCK: 0
LIBRI: 097 Print on Demand. Lieferbar innerhalb von 7 bis 10 Tagen * EK = ohne MwSt.
P_SALEALLOWED: WORLD
DRM: 0
0 = Kein Kopierschutz
1 = PDF Wasserzeichen
2 = DRM Adobe
3 = DRM WMA (Windows Media Audio)
4 = MP3 Wasserzeichen
6 = EPUB Wasserzeichen

UVP: 2 
Warengruppe: 16430 

KNO: 22668115
KNO-EK*: 157.13 € (25.00%)
KNO-VK: 320,99 €
KNV-STOCK: 0

KNO-SAMMLUNG: Notes on Numerical Fluid Mechanics and Multidisciplinary Design 92
P_ABB: Bibliographie
KNOABBVERMERK: 2006. xiv, 530 S. XIV, 528 p. Also available online. 235 mm
KNOMITARBEITER: Herausgegeben:Rath, Hans Josef; Holze, Carsten; Heinemann, Hans-Joachim; Henke, Rolf; Hönlinger, Heinz
Einband: Gebunden
Auflage: 2006
Sprache: Englisch
Beilage(n): HC runder Rücken kaschiert

Alle Preise inkl. MwSt., innerhalb Deutschlands liefern wir immer versandkostenfrei. Informationen zum Versand ins Ausland.

Kostenloser Versand*

innerhalb eines Werktages

OHNE RISIKO

30 Tage Rückgaberecht

Käuferschutz

mit Geld-Zurück-Garantie