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International Journal of Turbomachinery, Propulsion and Power, Volume 8, Issue 4

2023 December - 20 articles

Cover Story: The surge limit of centrifugal compressors is a key parameter in the design process of modern turbochargers. Since the extensive work of GREITZER and many other researchers in this field, it is well-known that surge is a system-dependent phenomenon. In the case of steady-state simulations, the simulation domain is chosen to be as small as possible due to the numerical cost. This simply implies that there is no system information included in the numerical model. Therefore, it is not possible to determine any system-dependent surge limit with today’s applied steady-state numerical methods. To overcome this issue, an enhanced GREITZER surge model, which has been developed at TU DARMSTADT, should act as a link between the simulation and the system in which the compressor will be operated. View this paper
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Articles (20)

  • Article
  • Open Access
3,118 Views
17 Pages

A growing significance of flexible steam turbine operation challenges the control of turbines, as part load operation using control valves can be accompanied by highly unsteady flow conditions. The increased dynamic load induced by pressure forces ca...

  • Feature Paper
  • Article
  • Open Access
4 Citations
3,359 Views
11 Pages

NREL-5MW Wind Turbine Noise Prediction by FWH-LES

  • Claudio Bernardi,
  • Federico Porcacchia,
  • Claudio Testa,
  • Pietro De Palma,
  • Stefano Leonardi and
  • Stefania Cherubini

This paper deals with large onshore wind turbine aeroacoustics. Noise from the NREL 5 MW device is predicted by the permeable-surface Ffowcs Williams–Hawkings equation (FWH-P), starting from the postprocessing of LES data on different acoustic...

  • Article
  • Open Access
2 Citations
5,509 Views
19 Pages

Fan Stage Design and Performance Optimization for Low Specific Thrust Turbofans

  • Oliver Sjögren,
  • Tomas Grönstedt,
  • Anders Lundbladh and
  • Carlos Xisto

In modern turbofan engines, the bypass section of the fan stage alone provides the majority of the total thrust required in cruise, and the size of the fan has a considerable effect on the overall engine weight and nacelle drag. Thrust requirements i...

  • Article
  • Open Access
6 Citations
2,944 Views
18 Pages

Helicopter and turboprop engines are susceptible to the ingestion of debris and other foreign objects, especially during take-off, landing, and hover. To avoid deleterious effects, filters such as Inlet Particle Separators (IPS) can be installed. How...

  • Article
  • Open Access
2 Citations
2,624 Views
14 Pages

Profile Loss Prediction for Organic Rankine Cycle Turbines: An Experimental Case Study

  • Leander Hake,
  • Stephan Sundermeier and
  • Stefan aus der Wiesche

The results of profile loss measurements, including trailing edge flow details, are presented for the flow of an organic vapor through a linear turbine cascade. The so-called VKI-I blade profile from the open literature was chosen for the cascade, an...

  • Article
  • Open Access
5 Citations
3,412 Views
12 Pages

Effect of Porosity and Injection Ratio on the Performance of Transpiration Cooling through Gyroids

  • Benjamin J. Brimacombe,
  • James A. Scobie,
  • Joseph M. Flynn,
  • Carl M. Sangan and
  • Oliver J. Pountney

This paper presents experimental measurements of adiabatic effectiveness for three transpiration cooling porosities (ϕ= 0.3, 0.4, and 0.5) constructed from gyroid lattice structures. To the authors’ knowledge, this is the first use of a Tr...

  • Article
  • Open Access
3,099 Views
12 Pages

Experimental and Numerical Investigation of a Turbine Vane Frame with Splitters at Different Operating Points

  • Simon Pramstrahler,
  • Andreas Peters,
  • Mikel Lucas García De Albéniz,
  • Peter Adrian Leitl,
  • Franz Heitmeir and
  • Andreas Marn

A turbine vane frame is a special type of intermediate turbine duct, and is one option to improve the efficiency and reduce the length and weight of an aero-engine. However, due to its geometry, it features a complex flow field, and therefore in-dept...

  • Article
  • Open Access
4 Citations
3,518 Views
13 Pages

Determination of a Numerical Surge Limit by Means of an Enhanced Greitzer Compressor Model

  • Tobias Haeckel,
  • Dominik Paul,
  • Sebastian Leichtfuß,
  • Heinz-Peter Schiffer and
  • Werner Eißler

The surge limit of centrifugal compressors is a key parameter in the design process of modern turbochargers. Numerical methods like steady-state simulations are state-of-the-art methods for predicting the performance of the centrifugal compressor. In...

  • Article
  • Open Access
10 Citations
3,827 Views
14 Pages

The Current Gap between Design Optimization and Experiments for Transonic Compressor Blades

  • Edwin Joseph Munoz Lopez,
  • Alexander Hergt,
  • Till Ockenfels,
  • Sebastian Grund and
  • Volker Gümmer

The successful design of compressor blades through numerical optimization relies on accurate CFD-RANS solvers that are able to capture the general performance of a given design candidate. However, this is a difficult task to achieve in transonic flow...

  • Article
  • Open Access
3 Citations
3,247 Views
11 Pages

A numerical method using combined detached-eddy simulation (DES) and a cavitation model considering the rotation effect is used for unsteady cavitation flow field of the centrifugal pump. A closed-type pump test system was established to obtain the p...

  • Feature Paper
  • Article
  • Open Access
1 Citations
2,374 Views
18 Pages

Grooved liquid annular seals have a significant influence on the design of turbomachines. Corresponding lubrication film models need to account for the different friction behavior of the grooves compared to plain seals. However, there is a lack of re...

  • Article
  • Open Access
3 Citations
2,189 Views
13 Pages

This paper presents the numerical characterization of a highly loaded compressor by means of 3D unsteady RANS simulations. The focus is on critical flow structures and their evolution at different operating points of the machine. First, the numerical...

  • Article
  • Open Access
3 Citations
2,767 Views
14 Pages

Surrogate Modeling of the Aeroacoustics of an NM80 Wind Turbine

  • Filippo De Girolamo,
  • Lorenzo Tieghi,
  • Giovanni Delibra,
  • Valerio Francesco Barnabei and
  • Alessandro Corsini

Wind turbines play a major role in the European Green Deal for clean energy transition. Noise is a critical aspect among open technological issues, as it determines the possibility of onshore installations near inhabited places and the possible detri...

  • Review
  • Open Access
6 Citations
3,740 Views
49 Pages

This paper aims to summarize the results of several experimental investigations regarding two-phase liquid–gas flows in radial centrifugal pumps. The main objective is to combine the corresponding experimental results and collect the obtained k...

  • Article
  • Open Access
8 Citations
3,628 Views
15 Pages

Adjoint-Based Design Optimization of a Volute for a Radial Compressor

  • Romain Hottois,
  • Arnaud Châtel and
  • Tom Verstraete

Numerical optimization methods are widely used for designing turbomachinery components due to the cost and time savings they can provide. In the available literature, the shape optimization of radial compressors mainly focuses on improving the impell...

  • Feature Paper
  • Article
  • Open Access
5 Citations
3,061 Views
14 Pages

New Supersonic Nozzle Test Rig Used to Generate Condensing Flow Test Data According to Barschdorff

  • Manuel Ernesto Maqueo Martínez,
  • Stefan Schippling,
  • Markus Schatz and
  • Damian M. Vogt

Considerable progress has been achieved in recent decades in understanding the phenomena related to the onset of condensation in steam flows, both experimentally and especially numerically. Nevertheless, there is still a certain disagreement between...

  • Feature Paper
  • Article
  • Open Access
2,499 Views
12 Pages

The head and flow rate of a pump characterize the pump performance, which help determine whether maintenance is needed. In the proposed method, instead of a traditional flowmeter and manometer, the operating points are identified using data collected...

  • Article
  • Open Access
1 Citations
2,359 Views
11 Pages

Transient Resonance Passage of a Mistuned Bladed Disk with and without Underplatform Dampers

  • Katharina Brinkmann,
  • Thomas Hoffmann,
  • Lars Panning-von Scheidt and
  • Heinrich Stüer

In this work, the vibration response of an academic free-standing turbine blisk is analyzed in regard to transient resonance passages. Measurement data are recorded using strain gauges and tip timing to evaluate the blades first bending mode both lin...

  • Article
  • Open Access
1 Citations
2,677 Views
10 Pages

For engines operating using heavy fuel oil (HFO), the nozzle rings of turbocharger turbines are prone to severe degradation because of contamination with unburned fuel deposits. This contamination may lead to increased excitation of blade resonance....

  • Article
  • Open Access
16 Citations
3,184 Views
15 Pages

The aerodynamics of a high-speed low-pressure turbine (LPT) cascade were investigated under steady and unsteady inlet flows. The tests were performed at outlet Mach (M) and Reynolds numbers (Re) of 0.90 and 70k, respectively. Unsteady wakes were simu...

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Int. J. Turbomach. Propuls. Power - ISSN 2504-186X