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Person

Eike Stumpf (1971-)

Maschinenbauingenieur

Name	Eike Stumpf
Time	1971- (Date of birth and death)
Place	Deutschland
Gender	männlich
Academic degree	Prof. Dr.-Ing.
Profession	Maschinenbauingenieur (characteristic profession) Hochschullehrer
Variant	E. Stumpf
Related	Rheinisch-Westfälische Technische Hochschule Aachen. Institut für Luft- und Raumfahrtsysteme
Further information	Universitätsprofessor am Lehrstuhl und Institut für Luft- und Raumfahrt der RWTH Aachen; Diss. Fachbereich Luft-und Raumfahrt
Record type	Person
GND-Identifier	128856084
Record ID	128856084
Involved in show all UNICADO software maintenance, revision, and management in a distributed collaboration Design of a low-emission long-range aircraft using UNICADO Enhancing UNICADO’s systems design methodology for future aircraft energy supply architectures A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany A methodology for variable camber assessment in conceptional aircraft design ASCLERA : DLR Design Challenge 2025 - MedEvac Aircraft Design process for a highly-efficient low-noise propeller Development of a generalized eVTOL vehicle cost model for Urban Air Mobility operations Development of design methodologies on the trailing edge architecture and application of variable camber to a segmented flap system Enhancing techno-economic assessments in aeronautic product development with systematic uncertainty management Enhancing UNICADO’s systems design methodology for future aircraft energy supply architectures Evaluation of system-level implications of introducing hydrogen-powered aircraft on the passenger air transportation network Gondelauslegung für Mantelpropellerantriebe Hybrid Rotor Noise Optimization Potential assessment of regional aircraft concepts with distributed hybrid-electric propulsion Public acceptance and safety assessment of urban air mobility in conceptual design Structural modelling and design strategies for lifting propellers Automatic safety model synthesis for aircraft conceptual design Automatic safety model synthesis for aircraft conceptual design Development of a mid fidelity aerodynamic analysis approach in the conceptual design of a tandem tiltwing eVTOL Experimental analysis of the interaction phenomena within closely spaced helical vortex pairs Optionen zur Umsetzung der Klimaschutzziele im Verkehrssektor Prediction of perceived annoyance caused by an electric drone noise through its technical, operational, and psychoacoustic parameters Preliminary design method for sizing and optimization of on-demand air mobility aircraft with distributed electric ducted fans along the wing leading edge Psychoacoustic optimization of the aviation noise of electric drones Simultaneous application of hybrid laminar flow control and variable camber in conceptual overall aircraft design Study On Public Acceptance of EVTOL: Safety & Noise Study On Public Acceptance of EVTOL: Safety & Noise Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments High-speed volumetric particle tracking measurements of unstable helical vortex pairs Experimental investigation of the acoustic emission of an electrically driven propeller in thrust and recuperation mode in a wind tunnel Bewertung elektrischer Systeme zur Verbesserung des Betriebsverhaltens von Flugtriebwerken Concept for a Hydrogen-Powered Aircraft for 150 Passengers with EIS 2035 Concept for a Hydrogen-Powered Aircraft for 150 Passengers with EIS 2035 Conceptual Design of a High-Altitude, Long-Endurance Aerial Vehicle System for Rapid Network Deployment Evaluation of electric propulsion systems in preliminary aircraft design Experimental investigation of the acoustic emission of an electrically driven propeller in thrust and recuperation mode in a wind tunnel Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments High-speed volumetric particle tracking measurements of unstable helical vortex pairs Influence of a Detailed Mass Estimation for a Wing with known Flight Shape in Conceptual Overall Aircraft Design influence of electric wing tip propulsion on the sizing of the vertical stabilizer and rudder in preliminary aircraft design Influence of electric wing tip propulsion on the sizing of the vertical stabilizer and rudder in preliminary aircraft design Investigation of small wind energy conversion systems under non-axial inflow conditions Kaskadierung für Flush Air Data Systeme Parameter Studies on Emissions and Costs of a Partial Turboelectric Commuter Aircraft SystemXF: a novel approach for holistic system modeling in aircraft conceptual design UNICADO: multidisciplinary analysis in conceptual aircraft design Correction to: Technology selection for holistic analysis of hybrid‑electric commuter aircraft Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber Technology selection for holistic analysis of hybrid-electric commuter aircraft Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level Combined Application of Hybrid Laminar Flow Control and Variable Camber in Preliminary Aircraft Design DLR Design Challenge 2022: Next Generation Firefighting Aircraft – FireWasp Electrical Drive and Regeneration in General Aviation Flight with Propellers Electrical propulsion systems for civil transportation aircraft Entwurfsmethode für elektrische und hybride Kleinflugzeugantriebe Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber

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Katalog der Deutschen Nationalbibliothek

Eike Stumpf (1971-)

UNICADO software maintenance, revision, and management in a distributed collaboration

Design of a low-emission long-range aircraft using UNICADO

Enhancing UNICADO’s systems design methodology for future aircraft energy supply architectures

A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany

A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany

A method to determine the availability and performance of fixed-wing air taxis in real weather conditions for regional air mobility within Germany

A methodology for variable camber assessment in conceptional aircraft design

ASCLERA : DLR Design Challenge 2025 - MedEvac Aircraft

Design process for a highly-efficient low-noise propeller

Development of a generalized eVTOL vehicle cost model for Urban Air Mobility operations

Development of design methodologies on the trailing edge architecture and application of variable camber to a segmented flap system

Enhancing techno-economic assessments in aeronautic product development with systematic uncertainty management

Enhancing UNICADO’s systems design methodology for future aircraft energy supply architectures

Evaluation of system-level implications of introducing hydrogen-powered aircraft on the passenger air transportation network

Gondelauslegung für Mantelpropellerantriebe

Hybrid Rotor Noise Optimization

Potential assessment of regional aircraft concepts with distributed hybrid-electric propulsion

Public acceptance and safety assessment of urban air mobility in conceptual design

Structural modelling and design strategies for lifting propellers

Automatic safety model synthesis for aircraft conceptual design

Automatic safety model synthesis for aircraft conceptual design

Development of a mid fidelity aerodynamic analysis approach in the conceptual design of a tandem tiltwing eVTOL

Experimental analysis of the interaction phenomena within closely spaced helical vortex pairs

Optionen zur Umsetzung der Klimaschutzziele im Verkehrssektor

Prediction of perceived annoyance caused by an electric drone noise through its technical, operational, and psychoacoustic parameters

Preliminary design method for sizing and optimization of on-demand air mobility aircraft with distributed electric ducted fans along the wing leading edge

Psychoacoustic optimization of the aviation noise of electric drones

Simultaneous application of hybrid laminar flow control and variable camber in conceptual overall aircraft design

Study On Public Acceptance of EVTOL: Safety & Noise

Study On Public Acceptance of EVTOL: Safety & Noise

Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments

High-speed volumetric particle tracking measurements of unstable helical vortex pairs

Experimental investigation of the acoustic emission of an electrically driven propeller in thrust and recuperation mode in a wind tunnel

Bewertung elektrischer Systeme zur Verbesserung des Betriebsverhaltens von Flugtriebwerken

Concept for a Hydrogen-Powered Aircraft for 150 Passengers with EIS 2035

Concept for a Hydrogen-Powered Aircraft for 150 Passengers with EIS 2035

Conceptual Design of a High-Altitude, Long-Endurance Aerial Vehicle System for Rapid Network Deployment

Evaluation of electric propulsion systems in preliminary aircraft design

Experimental investigation of the acoustic emission of an electrically driven propeller in thrust and recuperation mode in a wind tunnel

Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments

High-speed volumetric particle tracking measurements of unstable helical vortex pairs

Influence of a Detailed Mass Estimation for a Wing with known Flight Shape in Conceptual Overall Aircraft Design

influence of electric wing tip propulsion on the sizing of the vertical stabilizer and rudder in preliminary aircraft design

Influence of electric wing tip propulsion on the sizing of the vertical stabilizer and rudder in preliminary aircraft design

Investigation of small wind energy conversion systems under non-axial inflow conditions

Kaskadierung für Flush Air Data Systeme

Parameter Studies on Emissions and Costs of a Partial Turboelectric Commuter Aircraft

SystemXF: a novel approach for holistic system modeling in aircraft conceptual design

UNICADO: multidisciplinary analysis in conceptual aircraft design

Correction to: Technology selection for holistic analysis of hybrid‑electric commuter aircraft

Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber

Technology selection for holistic analysis of hybrid-electric commuter aircraft

Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

Combined Application of Hybrid Laminar Flow Control and Variable Camber in Preliminary Aircraft Design

DLR Design Challenge 2022: Next Generation Firefighting Aircraft – FireWasp

Electrical Drive and Regeneration in General Aviation Flight with Propellers

Electrical propulsion systems for civil transportation aircraft

Entwurfsmethode für elektrische und hybride Kleinflugzeugantriebe

Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber