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Home > New Results in Numerical and Experimental Fluid Mechanics: Contributions to the 10th AG STAB/DGLR Symposium Braunschweig, Germany 1996 > Parallel Numerical Airplane Wing Design
New Results in Numerical and Experimental Fluid Mechanics: Contributions to the 10th AG STAB/DGLR Symposium Braunschweig, Germany 1996 |
Horst Körner; Reinhard Hilbig
Vieweg+Teubner Verlag
New Results in Numerical and Experimental Fluid Mechanics: Contributions to the 10th AG STAB/DGLR Symposium Braunschweig, Germany 1996
Parallel Numerical Airplane Wing Design
Authors

J. K. Axmann; M. Hadenfeld; O. Frommann

ARI Id

1664222795698_821741

Access

Not Available Free

Pages

48-55

DOI

10.1007/978-3-322-86573-1_6

Chapter URL

https://rd.springer.com/chapter/10.1007/978-3-322-86573-1_6

Table of Contents of Book
Showing 1 to 20 of 55 entries
Chapters/HeadingsAuthor(s)PagesInfo
Front Matter
i-xii
Cooperation Project Aeronautical Research
H. Diehl
1-6
Reduction of Aerodynamic Drag (RaWid) in the national Research and Technology Programme for Aeronautics Status after the First Year of the Programme
Josef Mertens
7-14
National CFD Project MEGAFLOW
Norbert Kroll
15-23
Laminar-Turbulent Transition Research at DLR
Uwe Ch. Dallmann
24-35
The Development of Advanced Internal Balances for Cryogenic and Conventional Tunnels
B. Ewald; K. Hufnagel
36-47
Parallel Numerical Airplane Wing Design
J. K. Axmann; M. Hadenfeld; O. Frommann
48-55
Experiments on Active Control of Tollmien—Schlichting Waves on a Wing
M. Baumann; W. Nitsche
56-63
Stability Analysis of two- and three-dimensional Boundary Layer Flows with varied Wall Temperatures
F. P. Bertolotti; H. Bieler
64-70
Heat Loads During Hypersonic -Flight-Conditions at Low Altitudes: Computations and Free-Flight Investigations of Several Testdomes
F. St. Boller; P. G. Fisch; A. Merten; K. Moldenhauer
71-78
Experimental Studies of the Turbulent Flow Structure of Leading—Edge Vortices
Chr. Breitsamter
79-86
Density Measurements on a Delta Wing by Means of Planar Intensity Distribution of Rayleigh Scattered Laser Light (PIRS) in the 1m × 1m Transonic Wind Tunnel Göttingen (TWG)
K. A. Bütefisch; V. Schmidt; H. Vollmers; A. Luczak; V. Beushausen; G. Wolfrum et al.
87-94
Close Coupling of Very High-Bypass Engines in Combination with Take-Off / Landing Configurations
W. Burgsmüller; S. Thomé
95-102
Numerical investigation of boundary-layer instabilities over a blunt flat plate at angle of attack in supersonic flow
Guido Dietz; Alexander Meijering
103-110
Application of Two-Parameter Turbulence Models to the Prediction of Two-Dimensional Free Turbulent Shear Flows
B. Dreßler
111-118
Numerical and Experimental Investigations of Flow Induced by Harmonic Motion of a Circular Cylinder
H. Dütsch; S. Becker; H. Lienhart
119-126
Status and some new results obtained in the HEG
G. Eitelberg; R. Krek; N. Widdecke; W. H. Beck
127-134
Mesh Modification Techniques for Navier-Stokes Meshes
E. Elsholz; H. Steinmeyer
135-142
Flight experiment guidance technique for research on transition with Grob G109 aircraft of the Technische Hochschule Darmstadt
P. Erb; B. Ewald; M. Roth
143-150
Alternative drag calculations from off body flow quantities using the FLOWer code
B. Ewald; P. Kreuzer
151-156
Chapters/HeadingsAuthor(s)PagesInfo
Showing 1 to 20 of 55 entries
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