direkt zum Inhalt springen

direkt zum Hauptnavigationsmenü

Sie sind hier

TU Berlin

Inhalt des Dokuments

Publikationen am Fachgebiet Luftfahrtantriebe

2017

[104] Numerical investigation of virtual control surfaces for vibration control on compressor blades

V. Motta, L. Malzacher, D. Peitsch
(TU Berlin)

IFASD-2017 International Forum on Aeroelasticity and Structural Dynamics,
Como, Italy, June 25-28 2017, IFASD-2017-137


[103] Numerical assessment of virtual control surfaces for compressor blades

V. Motta, L. Malzacher, P. Neumann, D. Peitsch
(TU Berlin)

35th AIAA Applied Aerodynamics Conference,
Denver, USA, June 5-9 2017, AIAA 2017-3909


[102] Physics of prestall propagating disturbances in axial compressors and their potential as a stall warning indicator


M. Eck, S. Geist, D. Peitsch
(TU Berlin)

Journal of Applied Sciences, Gas Turbines Propulsion and Power, MDPI, 2017


[101] Advanced stereo high-speed PIV in an annular cascade without clearance: evidence of Rotating Instability


J. Peter, B. Pardowitz, M. Eck, L. Enghardt, D. Peitsch, P.U. Thamsen

12th European Turbomachinery Conference, ETC 12,
Stockholm, Sweden, April 3-7 2017, ETC2017-205


Nach oben

2016

[100] Betriebspunktabhängige Kühlluftführung für Gasturbinen

D. Woelki, D. Peitsch
(TU Berlin)

Abschlussbericht AG Turbo 2020 3.1.4, FKZ 03ET2013P
Technische Universität Berlin, 2016


[99] Fan casing contouring under consideration of aeroacoustics, mechanics, aeroelasticity and whole engine performance

A.-L. Aulich1, T. Sauer2, S. Iseni3, A. Moreau4, D. Peitsch2, R. Mailach3, D. Micallef3, L. Enghardt4, E. Nicke1

(1 Deutsches Zentrum für Luft und Raumfahrt (DLR), Köln; 2 Technische Universität Berlin (TUB), Berlin; 3 Ruhr-Universität Bochum (RUB), Bochum; 4 Deutsches Zentrum für Luft und Raumfahrt (DLR), Berlin)

CEAS Aeronautical Journal, 2016, DOI 10.1007/s13272-016-0226-z


[98] 3D Numerical and Experimental Investigation of High Turning Compressor
Tandem Cascades


J. Eckel, A. Heinrich, C. Janke, J. Ortmanns, D. Peitsch

Deutscher Luft- und Raumfahrtkongress 2016,
Braunschweig, Germany, September 13-15 2016, DLRK 2016-420320


[97]
A low Speed Compressor Test Rig for Flutter Investigations


L. Malzacher1, S. Geist1, D. Peitsch1, H. Hennings2
(1 TU Berlin, 2 DLR Göttingen)

ASME Turbo Expo 2016,
Seoul, South Korea, June 13-17 2016, GT2016-57960


[96] Experimental Investigations on Highly Loaded Compressor Airfoils with Active Flow Control under Non-Steady Flow Conditions in a 3d-Annular Low-Speed Cascade

C. Brück, C. Tiedemann, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2016,
Seoul, South Korea, June 13-17 2016, GT2016-56891


[95] Investigation of Bypass Transition in the Presence of a Separation Bubble
with tomographic PIV


C. Lyko1, D. Peitsch1, D. Michaelis2, M. Dittmar2
(1 TU Berlin, 2 LaVision GmbH Göttingen)

ASME Turbo Expo 2016,
Seoul, South Korea, June 13-17 2016, GT2016-57884


[94] Enhanced convective Heat Transfer due to dynamically forced Impingement Jet Arrays

F. Haucke, W. Nitsche, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2016,
Seoul, South Korea, June 13-17 2016, GT2016-57360


Nach oben

2015

[93] An Automated Process to Create Start Values for Gas Turbine Performance Simulations Using Neural Networks and Evolutionary Algorithms

R. Becker1, M. Bolemant2, D. Krause2, D. Peitsch2
(1 Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR); 2 TU Berlin)

International Gas Turbine Congress 2015,
Tokyo, Japan, November 15-20 2015, IGTC2015-0107


[92] Flexibilization of compressor and turbine characteristics for optimized specification in off-design condition


T. Sauer, D. Peitsch
(TU Berlin)

International Gas Turbine Congress 2015,
Tokyo, Japan, November 15-20 2015, IGTC2015-0095


[91] Interaction of Main Flow and Sealing Air across a Turbine Cavity under unsteady conditions


T. Schliwka, C. Tiedemann, D. Peitsch
(TU Berlin)

22th ISABE, International Symposium on Air Breathing Engines,
Phoenix, Arizona, USA, October 25-30 2015, ISABE-2015-21288


[90] Rotierende Instabilität in Axialverdichtern – Experimente und Analysemethoden zur Untersuchung instationärer 3D Wirbelstrukturen


M. Eck, D. Peitsch, J. Peter, P. U. Thamsen, B. Pardowitz, L. Enghardt

20 Jahre NGV Dresden - Forschung zur Verdichteraerodynamik,
Dresden, Germany, October 6-7 2015


[89] Fan casing contouring under consideration of aeroacoustics, mechanics, aeroelasticity and whole engine performance

A.-L. Aulich1, T. Sauer2, S. Iseni3, A. Moreau4, D. Peitsch2, R. Mailach3, D. Micallef3, L. Enghardt4, E. Nicke1

(1 Deutsches Zentrum für Luft und Raumfahrt (DLR), Köln; 2 Technische Universität Berlin (TUB), Berlin; 3 Ruhr-Universität Bochum (RUB), Bochum; 4 Deutsches Zentrum für Luft und Raumfahrt (DLR), Berlin)

Deutscher Luft- und Raumfahrtkongress 2015,
Rostock, Germany, September 22-24 2015, DLRK 2015-370127


[88]
Detailed measurements of the unsteady pressure field in the area of origin of Rotating Instability

M. Eck, C. Tiedemann, D. Peitsch
(TU Berlin)

ISUAAAT 14,
Stockholm, Sweden, September 8-11 2015


[87] Facing the new challenges in the design of modern turbomachinery


D. Peitsch
(TU Berlin)

Polish Academy of Sciences,
Gdansk, Poland, June 25 2015


[86] Using the Unsteadiness - Game Changing Approaches in Gas Turbine Design


D. Peitsch
(TU Berlin)

PTNSS VI International Congress on Combustion Engines,
Olsztyn, Poland, June 22 2015


[85] Analysis of Laminar-Turbolent Transition of a Low-Loss Generic Low Pressure Turbine Distribution


C. Brück1, C. Lyko1, D. Peitsch1, C. Bode2, J. Friedrichs2, D. Kozulovic3, A. Fiala4,
Y. Guendogdu4

(1 TU Berlin, 2 TU Braunschweig, 3 HAW Hamburg, 4 MTU München)

ASME Turbo Expo 2015,
Montreal, Canada, June 15-19 2015, GT2015-42824


[84] Experimental Investigations of Secondary Flow Development around Tandem Vanes in a 2D Linear Stator Compressor Cascade

A. Heinrich, C. Tiedemann, D. Peitsch
(TU Berlin)

11th European Turbomachinery Conference, ETC 11,
Madrid, Spain, March 23-27 2015, ETC2015-237


Nach oben

2014

[83] Three-Dimensional Flow Field in Highly Loaded Compressor Cascade

C. Beselt, M. Eck, D. Peitsch
(TU Berlin)

Journal of Turbomachinery, Vol. 136, Issue 10, S. 101007-1 - 101007-10
October 2014


[82] Modellierung variabler Sekundärluftsysteme zur Bewertung ihrer Auswirkungen auf das Gesamtsystem Gasturbine


D. Woelki, D. Peitsch
(TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2014,
Augsburg, Germany, September 16-18 2014, DLRK 2014-340112


[81] An alternative compressor modeling method within gas turbine performance simulations


M. Bolemant, D. Peitsch
(TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2014,
Augsburg, Germany, September 16-18 2014, DLRK 2014-340047


[80] Experimental investigation of a turbine sealing cavity exposed to free stream pressure fluctuation


T. Schliwka, L. Malzacher, S. Chemnitz, D. Peitsch
(TU Berlin)

Active Flow and Combustion Control 2014,
Berlin, Germany, September 10-12 2014


[79] Three dimensional flow field in a highly loaded compressor cascade


C. Beselt, M. Eck, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2014
Düsseldorf, Germany, June 16-20 2014, GT2014-25947


[78] Experimental and numerical investigation of the unsteady endwall flow in a highly loaded axial compressor stator

C. Beselt, R. van Rennings, D. Peitsch, F. Thiele, K. Ehrenfried
(TU Berlin)

ASME Turbo Expo 2014
Düsseldorf, Germany, June 16-20 2014, GT2014-25944


[77]
Experimental investigation of secondary flow in an annular compressor stator cascade

M. Eck
(TU Berlin)

10th AIAA-PEGASUS Student Conference
Prague, Czechia, April 23-25 2014


[76] Simulation and validation of low pressure turbine transition parameters

L. Malzacher, C. Lyko, D. Peitsch
(TU Berlin)

15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC-15
Honolulu, Hawaii, USA, February 24-28 2014, ISROMAC-TU308


[75] A new linear high speed compressor stator cascade for tandem configurations


A. Heinrich, C. Tiedemann, D. Peitsch
(TU Berlin)

15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC-15
Honolulu, Hawaii, USA, February 24-28 2014, ISROMAC-FR307


Nach oben

2013

[74] Determination of the pressure distribution and fluctuations of the transonic flow in a highly loaded compressor cascade

K. Hummel, C. Tiedemann, D. Peitsch
(TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2013,
Stuttgart, Germany, September 10-12 2013, DLRK 2013-301482


[73]
Die Entwicklung einer Mess-Strecke mit optischem Zugang für den Heiß-Akustik-Teststand in Berlin


T. Schliwka, L. Malzacher, D. Peitsch
(TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2013,
Stuttgart, Germany, September 10-12 2013, DLRK 2013-301366


[72] Identification of surrogate control variables for a robust active flow controller of an experimental high speed stator cascade

S. Steinberg, C. Tiedemann, R. King, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2013,
San Antonio, USA, June 3-7 2013, GT2013-94179


[71] Forcing of separation bubbles by main flow unsteadiness or pulsed vortex generating jets - a comparison

C. Lyko, J. Dähnert, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2013,
San Antonio, USA, June 3-7 2013, GT2013-94575


[70] Impact of hub clearance on endwall flow in a highly loaded axial compressor stator

C. Beselt, R. van Rennings, D. Peitsch, F. Thiele
(TU Berlin)

ASME Turbo Expo 2013,
San Antonio, USA, June 3-7 2013, GT2013-95463


[69]
Influence of clearance size on rotating instability in an axial compressor stator

C. Beselt, B. Pardowitz, R. van Rennings, R. Sorge, D. Peitsch, L. Enghardt, F. Thiele, K. Ehrenfried, P. U. Thamsen
(TU Berlin, Deutsches Zentrum für Luft- und Raumfahrt e. V.)

10th European Turbomachinery Conference, ETC 10,
Lappeenranta, Finland, April 15–19 2013, ETC10-A141


[68] Experimental investigation of endwall flow in highly loaded annular compressor stator cascade

C. Beselt, D. Peitsch
(TU Berlin)

10th European Turbomachinery Conference, ETC 10,
Lappeenranta, Finland, April 15–19 2013, ETC10-A152


[67]
Transition mechanisms in laminar separated flow under simulated low pressure turbine aerofoil conditions

J. Dähnert, C. Lyko, D. Peitsch

Journal of Turbomachinery, Vol. 135, Issue 1, S. 011007-1 - 011007-10
January 2013


Nach oben

2012

[66] Powering the World – High Technology in Gas Turbines

D. Peitsch
(TU Berlin)

Invited Lecture, Conference‚ Rozwój Techniki, Technologii i Transportu w Lotnictwie,
Poznan, Poland, September 17-18 2012


[65]
Identifikation einer Regelgröße zur aktiven Strömungskontrolle an einer linearen Verdichterkaskade im kompressiblen Machzahlbereich

C. Tiedemann, S. Steinberg, D. Peitsch, R. King
(TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2012,
Berlin, Germany, September 10-12 2012, DLRK 2012-281267


[64] Some Aspects on Wet Compression - Physical Effects and Modeling Strategies used in Engine Performance Tools

M. Obermüller, K.-J. Schmidt, H. Schulte, D. Peitsch
(MTU Aero Engines, TU Berlin)

Deutscher Luft- und Raumfahrtkongress 2012,
Berlin, Germany, September 10-12 2012, DLRK 2012-281210


[63] A new linear high speed compressor stator cascade for active flow control investigations

C. Tiedemann, A. Heinrich, D. Peitsch
(TU Berlin)

6th AIAA Flow Control Conference,
New Orleans, USA, June 25-28 2012, AIAA-2012-3251


[62]
Experimental and numerical investigation of rotating instability phenomenon in an axial compressor stator

C. Beselt, D. Peitsch, R. van Rennings, F. Thiele
(TU Berlin)

42nd AIAA Fluid Dynamics Conference,
New Orleans, USA, June 25-28 2012, AIAA-2012-2980


[61] On the effect of volute tongue design on radial turbine performance

J. Suhrmann, D. Peitsch, M. Gugau, T. Heuer
(TU Berlin, BorgWarner Turbo Systems Engineering GmbH)

ASME Turbo Expo 2012,
Kopenhagen, Denmark, June 11-15 2012, GT2012-69525


[60]
Influence of mach number and aerodynamic loading on rotating instability in an annular compressor cascade

C. Beselt, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2012,
Kopenhagen, Denmark, June 11-15 2012, GT2012-69393


Nach oben

2011

[59] Transition Mechanisms in Laminar Separated Flow under Unsteady Main Flow Conditions - Part I: Steady Flowfield

C. Lyko, J. Dähnert, D. Peitsch
(TU Berlin)

IGTC 2011, International Gas Turbine Congress,
Osaka, Japan, November 13-18 2011, IGTC2011-0254


[58] Transition Mechanisms in Laminar Separated Flow under Unsteady Main Flow Conditions - Part II: Unsteady Flowfield

C. Lyko, J. Dähnert, D. Peitsch
(TU Berlin)

IGTC 2011, International Gas Turbine Congress,
Osaka, Japan, November 13-18 2011, IGTC2011-0255


[57] Validation and development of models for optimum wheel flow inlet angles of small size radial turbines

J. Suhrmann, D. Peitsch, M. Gugau, T. Heuer
(TU Berlin, BorgWarner Turbo Systems Engineering GmbH)

IGTC 2011, International Gas Turbine Congress,
Osaka, Japan, November 13-18 2011, IGTC2011-162-1


[56] Validation and development of models for optimum wheel flow outlet angles of small size radial turbines

J. Suhrmann, D. Peitsch, M. Gugau, T. Heuer
(TU Berlin, BorgWarner Turbo Systems Engineering GmbH)

IGTC 2011, International Gas Turbine Congress,
Osaka, Japan, November 13-18 2011, IGTC2011-162-2


[55] Strömungsinduzierter Schall in Turbomaschinen – Die Rotierende Instabilität

C. Beselt, D. Peitsch, B. Pardowitz, L. Enghardt
(TU Berlin, Deutsches Zentrum für Luft- und Raumfahrt e. V.)

Deutscher Luft- und Raumfahrtkongress 2011,
Bremen, Germany, September 27-29 2011, DLRK 2011-241377


[54]
Challenges for the Development of advanced Propulsion Systems for Aircraft

D. Peitsch
(TU Berlin)

International Congress on Thermodynamics,
Posen, Poland, September 4-7 2011


[53] Propelling the future - The meaning of ACARE VISION 2050 for the future development of propulsion systems for aircraft

D. Peitsch
(TU Berlin)

Invited Lecture, 4th International Congress on Combustion Engines,
Radom, Poland, June 16-17 2011, PTNSS-2011-SS4-401


[52] Transition mechanisms in laminar separated flow under simulated low pressure turbine aerofoil conditions


J. Dähnert, C. Lyko, D. Peitsch
(TU Berlin)

ASME Turbo Expo 2011,
Vancouver, Canada, June 6-10 2011, ASME GT2011-45690


[51] Hot-Acoustic-Testrig (HAT) - A unique facility for thermoacoustic research


K. Knobloch, C. Lahiri, L. Enghardt, F. Bake, D. Peitsch
(Deutsches Zentrum für Luft- und Raumfahrt e. V., TU Berlin)

ASME Turbo Expo 2011,
Vancouver, Canada, June 6-10 2011, ASME GT2011-45705


[50] Supporting the flying future - Research at the Institute for Aeronautics and Astronautics of TU Berlin


D. Peitsch
(TU Berlin)

Invited Lecture, Poznan University of Technology
Poznan, Poland, March 31 2011


Nach oben

2010

[49] Missionsabhängige Anpassung des Sekundärluftsystems zur Verbesserung der Triebwerksleistung

D. Peitsch
(TU Berlin)

DGLR Deutscher Luft- und Raumfahrt- Kongress 2010,
Hamburg, Germany, August 31 - September 02 2010, DLRK 2010-1214


[48] Validation and development of loss models for small size radial turbines


J. Suhrmann, D. Peitsch, M. Gugau, T. Heuer, U. Tomm
(TU Berlin, BorgWarner Turbo Systems Engineering GmbH)

ASME Turbo Expo 2010,
Glasgow, UK, June 14-18 2010, ASME GT2010-22666


[47] Detailed Design of a High Speed Switched Reluctance Starter/Generator for More/All Electric Aircraft


S. Shoujuna, L. Weiguoa, D. Peitsch, U. Schaefer

Chinese Journal of Aeronautics,
Volume 23, Issue 2, April 2010, Pages 216-226


Nach oben

2009

[46] JETSDREAM Entwicklung einer Kleingasturbine zur studentischen Ausbildung

D. Peitsch, A. Krumme, A. Pahs, K. Abu-Taa
(TU Berlin)

DGLR Deutscher Luft- und Raumfahrt- Kongress 2009,
Aachen, Germany, September 8-11 2009, DLRK 2009-1331


[45] Compressor Testing at AneCom AeroTest – Investigation of Surge
Characteristics of a 9-stage Axial Compressor


R. Geissler, D. Peitsch, D. Müller, V. Gümmer
(Anecom AeroTest GmbH and Rolls-Royce Deutschland Ltd & Co KG)

19th ISABE, International Symposium on Air Breathing Engines,
Montréal, Canada, September 7-11 2009, ISABE-2009-1223


[44] „Greening of Aeroengines“: Triebwerkskonzepte der Zukunft

D. Peitsch
(TU Berlin)

Ingenieurspiegel 1/2009, 22-23


Nach oben

2008

[43] Numerische Untersuchungen des Einflusses der Geometriekomplexität und der Transitionsmodellierung auf das Strömungsverhalten eines 4.5-stufigen Axialverdichters

P. Kupijai, M. Swoboda, B. Becker, A. Keskin, D. Peitsch

DGLR Deutscher Luft- und Raumfahrt- Kongress 2008,
Darmstadt, Germany, September 23-25 2008, DLRK 2008-81267


[42] Strahltriebwerke der zivilen Luftfahrt


D. Peitsch
(TU Berlin)

Ingenieurspiegel 1/2008, 4-5


Nach oben

2007

[41] Transient Modelling of Geartrains in Two-Shaft Aeroengines

D. Peitsch, R. Hanne, T. Hartmann
(Rolls-Royce Deutschland Ltd.& Co. KG)

18th ISABE, International Symposium on Air Breathing Engines,
Beijing, China, September 2-7 2007, ISABE-2007-1362


Nach oben

2006

[40] Mischungsverstärker in konstant gekreuzten Scherschichten und im Abgasblütenmischer

B. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2006,
Friedrichshafen, Germany, November 6-9 2006, DGLR-2006-096


[39] Filmkühlungsuntersuchungen in instationärer Strömung mit Ablöseblase

M. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2006,
Friedrichshafen, Germany, November 6-9 2006, DGLR-2006-194

Nach oben

2005

[38] Versuchsstand zur Erzeugung periodisch instationärer turbulenter Nachläufe ohne Geschwindigkeitsdefekt

G. Hofmann, L. Pietsch, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2005,
Friedrichshafen, Germany, September 26-29 2005, DGLR-2005-236


[37] Mischungsverbesserung in Abgasmischern von Turbostrahltriebwerken


B. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2005,
Friedrichshafen, Germany, September 26-29 2005, DGLR-2005-163


[36] Einfluss einer Ablöseblase auf die Temperaturverteilung und Filmkühleffektivität im filmgekühlten, periodisch instationären Strömungsfeld

M. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2005,
Friedrichshafen, Germany, September 26-29 2005, DGLR-2005-164


Nach oben

2004

[35] Response of a Transitional Separation to Main Flow Unsteadiness

A. Meyer, J. Hourmouziadis, M. Talan

NATO, Research and Technology Agency, Specialist´s Meeting,
Prague, Czech Republic, October 4-8 2004


[34] Enhancement of Mixing Effectiveness in Skewed Streams

B. Deinert, J. Hourmouziadis

ASME Turbo Expo 2004,
Vienna, Austria, June 14-17 2004, ASME 2004-GT-53074


[33] Film Cooling in Unsteady Flow with Separation Bubble

M. Deinert, J. Hourmouziadis

ASME Turbo Expo 2004,
Vienna, Austria, June 14-17 2004, ASME 2004-GT-53075


Nach oben

2003

[32] Filmkühlungsuntersuchungen in instationärer Strömung mit Ablöseblase

M. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2003,
München, Germany, November 17-20 2003, DGLR-2003-101


[31] Mischungsverstärker in gerader und gekreuzter Scherschicht


B. Deinert, J. Hourmouziadis

DGLR Deutscher Luft- und Raumfahrt- Kongress 2003,
München, Germany, November 17-20 2003, DGLR-2003-101


[30] Kelvin-Helmholtz Type Vortices in Unsteady Separation Bubbles

M. Talan, J. Hourmouziadis

16th ISABE, International Symposium on Air Breathing Engines,
Cleveland, Ohio, USA, September 1-5 2003, ISABE-2003-1085


[29] Phase Shift in Transitional Separation Bubbles

J. Hourmouziadis

Boundary Layer Transition and Unsteady Aspects of Turbomachinery Flows
Syracuse University, New York, USA, August 17-20, 2003


[28] A Multi-Component and Multi-Disciplinary Student Design Project within an International Academic and Industrial Collaboration


F. Mund, A. Kalfas, R. Abhari, Y. Turcan, J. Hourmouziadis, I. Trébinjac, A. Vouillarmet

ASME Gas Turbine & Aeroengine Congress,
Atlanta, Georgia, June 16-19 2003, ASME GT2003-38163

Nach oben

2002

[27] Characteristic regimes of Transitional Separation Bubbles in Unsteady Flow

M. Talan, J.Hourmouziadis

Flow, Turbulence and Combustion, Special Issue Unsteady Flow in Turbomachinery,
Kluwer Academic Publishers, 69 (2002) 3-4, pp. 207-227,


[26] Das Wiederanlegen der transienten Ablöseblase in Turbomaschinen

M. Talan, J.Hourmouziadis

Deutscher Luft- und Raumfahrtkongress,
Stuttgart, Germany, September 23-26 2002, DGLR-JT2002-070


Nach oben

2001

[25] Staged combustor optimisation in the environmental aicraft envelope

A. Wulff, J. Hourmouziadis

8th CEAS Eurpean Propulsion Forum,
Nottingham, UK, March 26-28, 2001


Nach oben

2000

[24] Das DFG Verbundvorhaben periodisch instationäre Strömung in Turbomaschinen

J. Hourmouziadis

Deutscher Luft- und Raumfahrtkongress,
Leipzig, Germany, September 18-21 2000, DGLR-JT2000-030


[23] Free stream unsteadiness and turbulence - what is the difference?

J. Hourmouziadis

Boundary Layer Transition and Unsteady Aspects of Turbomachinery Flows
Syracuse University, New York, USA, August 20-22, 2000


[22] Stability, transition and reattachment characteristics of a separation bubble in unsteady flow

J. Hourmouziadis

Boundary Layer Transition and Unsteady Aspects of Turbomachinery Flows
Syracuse University, New York, USA, August 20-22, 2000


[21] Beitrag zur hochbelasteten Schaufelgrenzschicht

W. Lou

Fortschritt-Berichte VDI, Reihe7, Nr.395, ISBN 3-18-339507-x
VDI Verlag, Düsseldorf, Germany 2000


[20] Die gekreuzte Scherschicht

N. Schröder

Fortschritt-Berichte VDI, Reihe7, Nr.380, ISBN 3-18-338007-2
VDI Verlag, Düsseldorf, Germany 2000


[19] Trailing Edge 3D Free Shear Layers

N. Schröder, G. Hofmann, J. Hourmouziadis

ASME TURBO EXPO 2000 Land, Sea & Air,
Munich, Germany May 08-11, 2000, 2000-GT-0436


[18] A Multimedia Aeroengine Design Course with Industry Support


J. Hourmouziadis, N. Schröder, K. Biegi, K.-J. Schmidt, S. Servaty, W. Gärtner

ASME TURBO EXPO 2000 Land, Sea & Air,
Munich, Germany May 08-11, 2000, 2000-GT-0585


[17] Separation Bubbles under Steady and Periodic-Unsteady Main Flow Conditions


W. Lou, J. Hourmouziadis

ASME TURBO EXPO 2000 Land, Sea & Air
Munich, Germany May 08-11, 2000, 2000-GT-0270


Nach oben

1999

[16] Industry Integrated Aeroengine Education at the Berlin University of Technology

W. Lou, J. Hourmouziadis

International Conference on Engineering Education,
Beijing, China, November 03-05, 1999


[15] Experimentelle Untersuchung der stationären und periodischen Plattengrenzschichten mit Ablöseblase

W. Lou, L. Willer, Y. Gündogdu, E. Ücgül, J. Hourmouziadis

Deutscher Luft- und Raumfahrtkongress DGLR-Jahrestagung 1999,
Berlin, Germany, September 27-30, 1999


[14] Experimentelle Untersuchungen der Strömung eines Abgasmischers

U. Strecker, J. Hourmouziadis

Deutscher Luft- und Raumfahrtkongress DGLR-Jahrestagung 1999,
Berlin, Germany, September 27-30, 1999


[13] Untersuchungen zum Stabilitätsverhalten von Verdichtungssystemen

R. Kühle, J. Hourmouziadis

Deutscher Luft- und Raumfahrtkongress DGLR-Jahrestagung 1999,
Berlin, Germany, September 27-30, 1999


[12] A Universal Combustor Model for the Prediction of Aeroengine Pollutant Emissions

A. Wulff, J. Hourmouziadis

14th International Symposium on Airbreathing Engines, IS-168,
Florence, Italy, September 05-10, 1999


[11] Experimental Investigation of Periodic-Unsteady Flat Plate Boundary Layers with Pressure Gradients

W. Lou, J. Hourmouziadis

3rd ASME/JSME Joint Fluids Engineering Conference, FED SM 99-7190,
San Francisco, USA, July 18-23, 1999

Nach oben

1998

[10] Combined Test Facility for Three-Dimensional Mixing Layer and Unsteady Boundary Layer Research

N. Schröder, W. Lou, J. Hourmouziadis

DGLR-Fachsymposium Strömungen mit Ablösung (STAB),
Berlin, Germany, November 10-12, 1998


[9] Analytische Untersuchung der Strömungsstabilität in verdichtenden Systemen

D. Reitebuch, W. Lou, J. Hourmouziadis

Zamm Z. Angew. Math. Mech., P607-615,
Germany 1998


[8] Application of Artificial Neural Networks in Engine Condition Monitoring

D. Schweng, J. Hourmouziadis

19th International Symposium on Aircraft Integrated Monitoring Systems (AIMS98)
Garmisch-Partenkirchen, Germany, May 04-07, 1998

Nach oben

1997

[7] Future Challenges in Turbomachinery Fluid Dynamics

J. Hourmouziadis

The Jean J. Ginoux Lecture, Von Karman Institute for Fluid Dynamics,
Brussels, Belgium, November 14th, 1997


[6] Modellierung des Verbrennungsprozesses in Gasturbinenbrennkammern zur Abschätzung des Schadstoff-Emissionsverhaltens

A. Wulff, J. Hourmouziadis

DGLR-Fachausschußsitzung Schadstoffarme Verbrennung in Fluggasturbinen,
TU Dresden, Dresden, Germany, November 06-07, 1997


[5] Technology Review of Aeroengine Pollutant Emissions

A. Wulff, J. Hourmouziadis

Aerospace Science and Technology, 97/08, P557-572,
Paris, France, August, 1997


[4] Design and Calibration of a Double Stream Wind Tunnel

N. Schröder, J. Hourmouziadis

Windtunnels and Wind Tunnel Test Techniques, CEAS European Forum,
Cambridge, P49.1-49.8, April, 1997


[3] Artificial Neural Networks in Engine Condition Monitoring

D. Schweng, J. Hourmouziadis

1997 European Propulsion Forum,
Berlin, Germany, March 12-14, 1997

Nach oben

1996

[2] Analytische Untersuchung der Strömungsinstabilität in Verdichtungssystemen

W. Lou, J. Hourmouziadis

DGLR-Jahrestagung,
Dresden, September 24-27, 1996, (DGLR-JT96-049)


[1] Status and Trends of Aeroengine Pollutant Emissions

J. Hourmouziadis, A. Wulff

20th Congress of the ICAS,
Sorrento, Napoli, Italy, September 8-13, 1996, ICAS-96-2.9.4

Nach oben

Zusatzinformationen / Extras

Direktzugang

Schnellnavigation zur Seite über Nummerneingabe

Postanschrift

Institut für Luft- und Raumfahrt
Luftfahrtantriebe
Sekr. F1
Marchstraße 12-14
D-10587 Berlin