June 14, 2024 | ASME Turbo Expo Conference 2024

Meet us at the Turbo Expo 2024

ASME Turbo Expo Turbomachinery Technical Conference & Exposition
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ASME Turbo Expo

We will be presenting over twenty scientific papers on our latest research in turbomachinery and propulsion technologies at the international ASME Turbo Expo, which will be held this year in London from 24 to 28 June. The conference will focus on the achievements and challenges of net-zero transformation in the aviation and energy sectors.

What steps must be taken to achieve the goal of net-zero emissions by 2050? At ASME Turbo Expo 2024, the Institute of Propulsion Technology of the German Aerospace Center (DLR) will be presenting a range of innovative solutions, including the use of new energy sources such as hydrogen and new propulsion concepts. We will show how we are contributing to the common roadmap for a sustainable and liveable future and look forward to discussing our approaches with experts from different disciplines. We cordially invite all conference participants to attend our presentations and exchange ideas with us. The full programme of the ASME 2024 Turbomachinery Technical Conference & Exposition is available here.

See us speaking at ASME Turbo Expo 2024

Autoren

Titel

Session

Datum und Uhrzeit

S. Gövert, J. Berger,

T. Lipkowicz, T. Soworka, C. Hassa, T. Behrendt,

B. Janus

Experimental and Numerical Investigation of Hydrogen Combustion in a Dual-Swirl Burner for Aero-Engine Applications

High Hydrogen I

04-05

Monday, June 24

8:00 AM - 10:00 AM

A. Görtz

B. Schneider

Step-by-Step Evaluation of the Fuel Switch From Kerosene to Hydrogen on the Thermodynamic Cycle in Gas Turbine Engines

Conceptual Design and Optimization I

01-02

Monday, June 24

8:00 AM - 10:00 AM

R. Becker, G. Kasperovich, P. Tiessen, J. Haubrich,

T. Behrendt, B. Janus

Fuel Thermal Management and Injector Part Design for LPBF Manufacturing

Additive Manufacturing 18-02

Monday, June 24  

1:30 PM - 3:30 PM

M. Kavvalos,

M. Mennicken, R. Schnell, M. Trost,

K. Kyprianidis (MDU)

On the Performance of Variable-Geometry Ducted E-Fans

Modelling, Simulation and Validation I

01-09

Monday, June 24

1:30 PM - 3:30 PM

D. Mimic (LU Hannover),

J. Mahlstedt (LU Han.),

F. Herbst

Improved Compressor Performance Prediction Using a Vortex-Reactive Turbulence-Model Extension

Turbulence modeling methods 1

34-10

Tuesday, June 25

8:00 AM - 10:00 AM

A. Karimian,

R. Schmidt (Rolls-Royce), C. Janke (Rolls-Royce)

Robust Optimization of a Compressor Blade Through Combination of an Adjoint-Based Multistart Approach and Global Gaussian Process Regression

Modelling, Simulation and Validation I

01-09

Tuesday, June 25

8:00 AM - 10:00 AM

M. Mennicken,

R. Schnell,

D. Kozulovic (UniBW München)

Assessment of a BLI-Tolerant Aft-Fan at Design and Near Stall Conditions - From Preliminary to Detailed Aerodynamic Design

Fan design methods 1

34-02

Tuesday, June 25

1:30 PM - 3:30 PM

C. Morsbach, M. Matha, R.G. Brakmann, S. Tabassum, M. Bergmann, M. Schroll, C. Willert,

E. Kügeler

Investigating the unsteady dynamics of a multi-jet impingement cooling flow using large eddy simulation

Impingement Cooling I 15-01

Tuesday, June 25

4:00 PM - 5:30 PM

S. Zenkner, F. Carvalho,

R. Brakmann, G. Goinis

Variable Cycle Engine Concepts and Component Technologies - An Overview

Whole Engine Performance and Novel Concepts

01-16

Tuesday, June 25

4:00 PM - 5:30 PM

J. Klinner, E. J. Munoz Lopez, A. Hergt, C. Willert

The unsteady shock-boundary layer interaction in a compressor cascade - Part 1: Measurements with time-resolved PIV

Compressor Secondary Flows and Interactions

40-03

Wednesday, June 26

8:00 AM - 10:00 AM

B. F. Klose, C. Morsbach, M. Bergmann,

E. J. Munoz Lopez,

A. Hergt, E. Kügeler

The Unsteady Shock-Boundary Layer Interaction in a Compressor Cascade – Part 2: High-Fidelity Simulation

Compressor Secondary Flows and Interactions

40-03

Wednesday, June 26

8:00 AM - 10:00 AM

P. Sivel, C. Frey,

H.-P. Kersken, E. Kügeler

A Low Mach Preconditioned Harmonic Balance Solver for Cavity Flutter Computations

Advanced Aeroelastic Prediction and Validation 22-03

Wednesday, June 26

8:00 AM - 10:00 AM

E. J. Munoz Lopez,

A. Hergt, J. Klinner,

B. F. Klose, C. Willert,

V. Guemmer

The unsteady shock-boundary layer interaction in a compressor cascade - Part 3: Mechanisms of shock oscillation

Compressor Secondary Flows and Interactions

40-3

Wednesday, June 26

8:00 AM - 10:00 AM

R. Meyer, U. Tapken,

U. Klähn, M. Behn,

T. Lengyel-Kampmann

Experimental and Numerical Investigation of the Counter-Rotating DLR turbo fan stage CRISPmulti with Boundary Layer Ingestion

Inlet Distortion

31-12

Wednesday, June 26

8:00 AM - 10:00 AM

R. Meyer, U. Tapken,

U. Klähn, M. Behn,

T. Lengyel-Kampmann

Unsteady Flow, Turbulence and Acoustic Measurements on the Counter-Rotating DLR Turbo Fan Stage Crispmulti, With and Without Inlet Distortions

Fan & Compressor Inflow Distortion Effects

40-04

Wednesday, June 26 10:30 AM - 12:00 PM

C. Frey, J. Backhaus,

G. Ashcroft, G. Geiser,

B. Winhart (MTU),

H. Stüer (Siemens Energy)

Using Pseudotime Marching for the Solution of Harmonic Balance Problems

Harmonic balance methods

34-05

Thursday, June 27

8:00 AM - 10:00 AM

G. Geiser,

F. Schwarzenthal,

G. Ashcroft, M. Hartmann (MTU), D. Schlüß (MTU)

On the Development of an Efficient Sliding Mesh Interface for the Harmonic Balance Method,

Part I: Implementation and Verification

Harmonic balance methods

34-05

Thursday, June 27

8:00 AM - 10:00 AM

M. Hartmann (MTU),

D. Schlüß (MTU),

G. Geiser,

F. Schwarzenthal,

G. Ashcroft,

F. Herbst

On the Development of an Efficient Sliding Mesh Interface for the Harmonic Balance Method,

Part II: Effects of Casing Treatments on the Aerodynamic Damping of a Compressor Blade

Harmonic balance methods

34-05

Thursday, June 27

8:00 AM - 10:00 AM

P. Weggler, J. Bachner,

F.-X. König, R. Stephan,

C. Gmeli

High Resolution Probe Measurements in a Multi-Stage Turbine Rig

Aerodynamic Studies

32-10

Thursday, June 27

8:00 AM - 10:00 AM

F.M. Möller, P.G. Tucker, Z.-N. Wang, C. Bode,

C. Morsbach, M. Matha,

P. Sivel

Advanced Methods for Assessing Flow Physics of the TU Darmstadt Compressor Stage:

Part 1 - Transitional Delayed Detached-Eddy Simulation

Turbulence modeling methods 2

34-18

Friday, June 28

8:00 AM - 10:00 AM

M. Matha, F.M. Möller,

C. Bode, C. Morsbach,

E. Kügeler

Advanced Methods for Assessing Flow Physics of the TU Darmstadt Compressor Stage:

Part 2 - Uncertainty Quantification of RANS Turbulence Modeling

Turbulence modeling methods 2

34-18

Friday, June 28

8:00 AM - 10:00 AM

T. Lipkowicz, S. Gövert,

B. Janus

Adaptation of the Low Dissipation Low Dispersion Scheme for Reactive Multi Component Flows on Unstructured Grids Using Density-Based Solvers

Combustion Modeling VI 04-18

Friday, June 28

8:00 AM - 10:00 AM

R. Brakmann, C. Pain,

F. Kocian, F. Carvalho,

C. Morsbach, M. Matha, M. Schroll, C. Willert

Fluidic Oscillators in Jet Impingement: A Numerical and Experimental Study on Heat Transfer Enhancement

Heat Transfer: Internal Cooling

 

Contact

Annabel Brückmann

Public Relations
German Aerospace Center (DLR)
Institute of Propulsion Technology
Linder Höhe, 50679 Köln
Tel: +4922036015080