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Konrad Vogeler

Observed names: K Vogeler, K. Vogeler, Konrad Vogeler,, Vogeler, K., Vogeler, Konrad
OpenAlex ID: A5078488993
Rotating Instabilities in an Axial Compressor Originating From the Fluctuating Blade Tip Vortex
2000 · R. Mailach, I. Lehmann, et al. · Journal of Turbomachinery · 340
Probabilistic CFD Simulation of a High-Pressure Compressor Stage Taking Manufacturing Variability Into Account
2010 · Alexander Lange, Matthias Voigt, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 85
Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the Endwall
2000 · H. Sauer, R. Müller, et al. · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 80
Reduction of Secondary Flow Losses in Turbine Cascades by Leading Edge Modifications at the Endwall
2000 · H. Sauer, R. Mu¨ller, et al. · Journal of Turbomachinery · 70
The Periodical Interaction of the Tip Clearance Flow in the Blade Rows of Axial Compressors
2001 · Ronald Mailach, Helmut Sauer, et al. · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 65
Impact of Manufacturing Variability on Multistage High-Pressure Compressor Performance
2012 · Alexander Lange, Matthias Voigt, et al. · Journal of Engineering for Gas Turbines and Power · 63
Introduction of a Parameter Based Compressor Blade Model for Considering Measured Geometry Uncertainties in Numerical Simulation
2009 · Alexander Lange, Konrad Vogeler, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 53
Impact of Manufacturing Variability and Nonaxisymmetry on High-Pressure Compressor Stage Performance
2012 · Alexander Lange, Matthias Voigt, et al. · Journal of Engineering for Gas Turbines and Power · 50
Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor—Part II: Wake-Tip Clearance Vortex Interaction
2008 · Ronald Mailach, Ingolf Lehmann, et al. · Journal of Turbomachinery · 47
Experimental and Numerical Investigation of a Circumferential Groove Casing Treatment in a Low-Speed Axial Research Compressor at Different Tip Clearances
2017 · Matthias Rolfes, Martin Lange, et al. · Journal of Turbomachinery · 44
Principal component analysis on 3D scanned compressor blades for probabilistic CFD simulation
2012 · Alexander Lange, Matthias Voigt, et al. · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 36
Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part I: Unsteady Profile Pressures and the Effect of Clocking
2004 · Ronald Mailach, Konrad Vogeler · Journal of Turbomachinery · 36
Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development
2004 · Ronald Mailach, Konrad Vogeler · Journal of Turbomachinery · 32
Aerodynamic Blade Row Interactions in an Axial Compressor: Part I — Unsteady Boundary Layer Development
2003 · Ronald Mailach, Konrad Vogeler · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 32
Experimental Investigation Into the Effects of the Steady Wake-Tip Clearance Vortex Interaction in a Compressor Cascade
2014 · Andreas Krug, Peter Busse, et al. · Journal of Turbomachinery · 31
Rotating Instabilities in an Axial Compressor Originating From the Fluctuating Blade Tip Vortex
2000 · R. Mailach, I. Lehmann, et al. · Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery · 29
A parametric model for probabilistic analysis of turbine blades considering real geometric effects
2013 · Kay Heinze, Marcus Meyer, et al. · CEAS Aeronautical Journal · 27
Analysis of High Pressure Turbine Nozzle Guide Vanes Considering Geometric Variations
2016 · Lars Högner, Alkin Nasuf, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 24
An Experimental Investigation of a Tandem Stator Flow Characteristic in a Low Speed Axial Research Compressor
2014 · Alrik Tesch, Martin Lange, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 24
Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor—Part I: Flow Field at Midspan
2008 · Ronald Mailach, Ingolf Lehmann, et al. · Journal of Turbomachinery · 22
An Experimental Verification of a New Design for Cantilevered Stators With Large Hub Clearances
2013 · Martin Lange, Konrad Vogeler, et al. · Journal of Turbomachinery · 21
The Potential of Sequential Combustion for High Bypass Jet Engines
1998 · Konrad Vogeler · Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery · 21
Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part II: Unsteady Aerodynamic Forces of Rotor and Stator Blades
2004 · Ronald Mailach, Lutz Mu¨ller, et al. · Journal of Turbomachinery · 18
Probabilistic Lifetime Analysis for Turbine Blades Based on a Combined Direct Monte Carlo and Response Surface Approach
2004 · Matthias Voigt, Roland Mu¨cke, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 18
Experimental and Numerical Investigation of a Circumferential Groove Casing Treatment in a Low Speed Axial Research Compressor at Different Tip Clearances
2017 · Matthias Rolfes, Martin Lange, et al. · ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT) · 17
Works count: 102
Citation count: 1,759
H-index: 21
I10-index: 44
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