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A. Eberle
Observed names:
A Eberle,
A. EBERLE,
Adrian Eberle,
Eberle, Adrian
Observed institutions:
Messerschmitt-Bölkow-Blohm (Germany),
National Aeronautics and Space Administration,
Airbus (Germany),
Daimler (Germany)
OpenAlex ID:
A5108359045
Numerical simulation of aeroacoustic sound generated by generic bodies placed on a plate. I - Prediction of aeroacoustic sources
1999
·
R. Hoeld
, A. Brenneis
, et al.
·
AIAA/CEAS Aeroacoustics Conference
·
58
3D-Euler calculations using characteristic flux extrapolation
1985
·
A. EBERLE
·
23rd Aerospace Sciences Meeting
·
23
Application of an Implicit Relaxation Method Solving the Euler Equations for Time-Accurate Unsteady Problems
1990
·
A. Brenneis
, A. Eberle
·
Journal of Fluids Engineering
·
21
Clean Aviation Ultra-Performance Wing (UP-Wing)
2024
·
Adrian Eberle
, Bruno Stefes
, et al.
·
AIAA SciTech Forum
·
19
Verification of an implicit relaxation method for steady and unsteady viscous and inviscid flow problems
1988
·
M. A. Schmatz
, A. Brenneis
, et al.
·
OpenGrey (Institut de l'Information Scientifique et Technique)
·
18
A finite volume method for calculating transonic potential flow around wings from the pressure minimum integral
1978
·
A. Eberle
·
NASA STI Repository (National Aeronautics and Space Administration)
·
12
PDF
Transonic Flow Computations by Finite Elements: Airfoil Optimization and Analysis
1979
·
A. Eberle
·
Springer eBooks
·
6
Parametric study of a switchable vortex generator for load alleviation in transonic conditions
2024
·
Luca Marino
, Ilias Kiat
, et al.
·
AIAA SciTech Forum
·
5
PDF
Application of the Euler method EUFLEX to a fighter-type airplane configuration at transonic speed
1992
·
S. HEISS
, A. EBERLE
, et al.
·
AIAA Applied Aerodynamics Conference
·
5
Three-Dimensional Parametric Analysis of a Switchable Vortex Generator for Aerodynamic Load Alleviation at Transonic Speeds
2025
·
Luca Marino
, Adrian Eberle
, et al.
·
AIAA SciTech Forum
·
3
Coupled Static and Dynamic Aeroelastic Simulations in Transonic and Supersonic Flow
2000
·
Martin Stettner
, Werner Haase
, et al.
·
3
Numerical methods for aerothermodynamic design of hypersonic space transport vehicles
1993
·
K. M. Wanie
, A. Brenneis
, et al.
·
3
CFD Contributions during Hypersonic Airplane Intake Design
1992
·
Norbert Bissinger
, A. Eberle
·
OpenGrey (Institut de l'Information Scientifique et Technique)
·
3
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions
2025
·
Luca Marino
, Ilias Kiat
, et al.
·
Journal of Aircraft
·
1
Comparison of one and two-equation models for traffic flow calculations
1995
·
A Brenneis
, P Konhaeuser
, et al.
·
Fluid Dynamics Conference
·
1
High order characteristic flux averaging for the solution of the Euler equations
1986
·
A. Eberle
, O. Schaefer
·
1
An Exact Hodographmethod for the Design of Supercritical Wingsections
1976
·
A. Eberle
·
Springer eBooks
·
1
Three-Dimensional Analysis of Vortex Generators for Load Alleviation at Transonic Speeds
2026
·
Luca Marino
, Adrian Eberle
, et al.
·
Journal of Aircraft
Advanced finite volume methods for the simulation of MPD propulsion
2000
·
J. Heiermann
, M. Auweter-Kurtz
, et al.
·
AIAA Plasmadynamics and Lasers Conference
Recent CFD enhancements for structured mesh Navier-Stokes and Euler solvers
1993
·
A. Eberle
·
AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Transonic Flow Computations by a Variational Principle Finite Element Method
1981
·
A. Eberle
·
Vieweg+Teubner eBooks
A finite element method for the computation of transonic flow past airfoils
1980
·
A. Eberle
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
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Works count:
23
Citation count:
183
H-index:
6
I10-index:
6
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