MARC details
000 -LEADER |
fixed length control field |
06442cam a22004574i 4500 |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20211105144036.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
020613s2002 gw a b 100 0 eng d |
010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
LC control number |
2002283437 |
011 ## - LINKING LIBRARY OF CONGRESS CONTROL NUMBER [OBSOLETE] |
Local cataloguing issues note |
Changed OCLC from 49286489 to 50859224 |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
3540426965 |
Qualifying information |
hd.bd. |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
9783540426967 |
Qualifying information |
hd.bd. |
035 ## - SYSTEM CONTROL NUMBER |
System control number |
(ATU)b10259661 |
035 ## - SYSTEM CONTROL NUMBER |
System control number |
(DLC) 2002283437 |
035 ## - SYSTEM CONTROL NUMBER |
System control number |
(OCoLC)50859224 |
040 ## - CATALOGING SOURCE |
Original cataloging agency |
DLC |
Language of cataloging |
eng |
Description conventions |
rda |
Modifying agency |
ATU |
042 ## - AUTHENTICATION CODE |
Authentication code |
lccopycat |
050 00 - LIBRARY OF CONGRESS CALL NUMBER |
Classification number |
TL570. |
Item number |
A493 2000 |
082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
629.1323 |
111 2# - MAIN ENTRY--MEETING NAME |
Meeting name or jurisdiction name as entry element |
AG STAB/DGLR Symposium |
Number of part/section/meeting |
(12th : |
Date of meeting or treaty signing |
2000 : |
Location of meeting |
Stuttgart, Germany) |
245 10 - TITLE STATEMENT |
Title |
New results in numerical and experimental fluid mechanics III : |
Remainder of title |
contributions to the 12th STAB/DGLR symposium, Stuttgart, Germany, 2000 / |
Statement of responsibility, etc. |
Siegfried Wagner [and others] (editors). |
264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE |
Place of production, publication, distribution, manufacture |
Berlin ; |
-- |
New York : |
Name of producer, publisher, distributor, manufacturer |
Springer, |
Date of production, publication, distribution, manufacture, or copyright notice |
[2002] |
264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE |
Date of production, publication, distribution, manufacture, or copyright notice |
©2002 |
300 ## - PHYSICAL DESCRIPTION |
Extent |
xii, 433 pages : |
Other physical details |
illustrations (some colour) ; |
Dimensions |
24 cm. |
336 ## - CONTENT TYPE |
Content type term |
text |
Content type code |
txt |
Source |
rdacontent |
337 ## - MEDIA TYPE |
Media type term |
unmediated |
Media type code |
n |
Source |
rdamedia |
338 ## - CARRIER TYPE |
Carrier type term |
volume |
Carrier type code |
nc |
Source |
rdacarrier |
490 1# - SERIES STATEMENT |
Series statement |
Notes on numerical fluid mechanics, |
International Standard Serial Number |
0179-9614 ; |
Volume/sequential designation |
v. 77 |
504 ## - BIBLIOGRAPHY, ETC. NOTE |
Bibliography, etc. note |
Includes bibliographical references. |
505 00 - FORMATTED CONTENTS NOTE |
Title |
Design Work for the A3XX High-Lift-Wing -- |
-- |
Recent Improvements in the Measurement of Aerodynamic Damping Derivatives -- |
-- |
Calculation of Horizontal Stabilizer Efficiency with a Navier-Stokes Code -- |
-- |
3D RANS Simulations for High-Lift Analysis of Transport Aircraft Configurations -- |
-- |
Numerical Investigation of the Reynolds-Number-Effect on the Setting Sensitivity of a 2D High-Lift Multi-Element Airfoil -- |
-- |
Separation Control on a High-Lift Configuration by Periodic Exitation -- |
-- |
Numerical Investigation of the Effect of the High-Lift Configuration of a Transport Aircraft on its Vortex Wake -- |
-- |
The Relationship Between Near- and Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings -- |
-- |
Influence of Different Flap Settings on the Hazard Posed to Following Aircraft -- |
-- |
Numerical Simulation of Wake-Vortex Encounters Using the Chimera-Technique -- |
-- |
Aspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation -- |
-- |
Coupling of DLR Navier-Stokes Solver FLOWer with an e[superscript N]-Database Method for Laminar-Turbulent Transition Prediction on Airfoils -- |
-- |
Unsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Gottingen (DNW-TWG) -- |
-- |
Turbulence Modeling for Reentry-Vehicles -- |
-- |
Computation of the Two-Dimensional Flow in SERN Nozzles -- |
-- |
Experimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC -- |
-- |
Aerodynamic Analysis of the Dual-Mode Ramjet Vehicle JAPHAR -- |
-- |
Study of Shock-Wave/Boundary-Layer Interaction Flowfield on a 24[superscript [degree]] Ramp Model -- |
-- |
Numerical Investigations of Small-Amplitude Disturbances in a Laminar Boundary Layer with Impinging Shock Waves -- |
-- |
Surface Temperature Effects on Shock-Wave Boundary-Layer Interaction of Ramp Flows -- |
-- |
Preliminary Results of Numerical Simulations of Elastic Panels in Transonic Flows -- |
-- |
Numerical Simulation of Laminar Separation-Bubble Control -- |
-- |
On the Structure of Turbulence in the Transition Cylinder Wake -- |
-- |
Investigation of Subgrid-Scale Models in LES of Turbulent Flows with Separation -- |
-- |
Experimental and Numerical Investigations on Transition in a Laminar Separation Bubble -- |
-- |
Boundary-layer Separation Computed by Second-Moment Closure Models -- |
-- |
Experimental Investigation on the Behaviour of Disturbances Emitted from a Point Source in a Laminar Boundary Layer -- |
-- |
Experimental/Numerical Investigation of the Influence of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of an Airfoil -- |
-- |
Interference of Wave Trains with Varying Phase Relations in a Decelerated Two-Dimensional Boundary Layer -- |
-- |
Secondary Instability of Steady and Unsteady Crossflow Waves -- |
-- |
Examination of the Eddy-Viscosity Concept Regarding its Physical Justification -- |
-- |
A Numerical Method for Compressible and Low Mach Number Fluid Flow -- |
-- |
Turbulent Two-Dimensional Flow Around a Flexible Membrane Airfoil -- |
-- |
Solution of the Euler Equations on Locally Adaptive B-Spline Grids -- |
-- |
An Algorithm to Treat Flows Bounded by Arbitrarity Shaped Surfaces with Cartesian Meshes -- |
-- |
Grid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI -- |
-- |
Convergence Acceleration on Unstructured Meshes -- |
-- |
Enhancement of a Navier-Stokes Flow Solver for Patched Grids with Non-Coincident Grid Nodes -- |
-- |
Flow and Turbulence Structures in the Wake of a Simplified Car Model (Ahmed Modell) -- |
-- |
Flow Visualisation, Pressure Measurements and Numerical Calculations on Spike-Tipped Bodies -- |
-- |
Tip-Vortices in Transonic Axial-Compressors -- |
-- |
Airframe Noise - Generation and Reduction - a Report on Status and Perspectives of DLR-Research -- |
-- |
Receptivity of Three-Dimensional Boundary Layers to Roughness and Suction - Linear and Nonlinear Effects -- |
-- |
Active Control of Tollmien-Schlichting Instabilities by Multi-Channel Sensor Actuator Systems -- |
-- |
Time Resolved 2D Measurement Techniques for Quantitative Determination of Flow Fields and Surface Pressure Distributions -- |
-- |
Investigation of Transitional Structures in Artificially and Disturbed Excited Flat Plate Boundary Layer Flows Using Stereo and Multi-Plane PIV -- |
-- |
The Meaning of Disturbance Fields in Transition Experiments and Their Detection in the Test Section Flow of a Short Duration Wind Tunnel -- |
-- |
Surface Fence with an Integrated, Piezoresistive Pressure Sensor for Measurements of Static and Dynamic Wall Shear Stress -- |
-- |
Experimental Investigation of the Flow Close to the Surface of a High Lift Airfoil Configuration in a Large Wind Tunnel -- |
-- |
Detection of Density Gradients at Helicopter Rotor Blades in Flight. |
588 ## - SOURCE OF DESCRIPTION NOTE |
Source of description note |
Machine converted from AACR2 source record. |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Aerodynamics |
Form subdivision |
Congresses |
9 (RLIN) |
693834 |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Airplanes |
General subdivision |
Design and construction |
Form subdivision |
Congresses |
9 (RLIN) |
786228 |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Fluid dynamics |
Form subdivision |
Congresses |
9 (RLIN) |
690211 |
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Turbulence |
Form subdivision |
Congresses |
9 (RLIN) |
693839 |
700 1# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Wagner, Siegfried, |
Titles and other words associated with a name |
Dr. Ing. |
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE |
Uniform title |
Notes on numerical fluid mechanics ; |
Volume/sequential designation |
v. 77. |
9 (RLIN) |
233862 |
907 ## - LOCAL DATA ELEMENT G, LDG (RLIN) |
a |
.b10259661 |
b |
09-11-17 |
c |
27-10-15 |
998 ## - LOCAL CONTROL INFORMATION (RLIN) |
-- |
b |
-- |
c |
Operator's initials, OID (RLIN) |
06-04-16 |
Cataloger's initials, CIN (RLIN) |
m |
First date, FD (RLIN) |
a |
-- |
eng |
-- |
gw |
-- |
0 |
945 ## - LOCAL PROCESSING INFORMATION (OCLC) |
a |
629.1323 AGS |
g |
1 |
i |
A287308B |
j |
0 |
l |
cmain |
o |
- |
p |
$391.86 |
q |
- |
r |
- |
s |
- |
t |
0 |
u |
2 |
v |
0 |
w |
0 |
x |
0 |
y |
.i10612634 |
z |
28-10-15 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Book |