Veröffentlichungen

 

Stuttgarter Profilkataloge als pdf erhältlich! Weitere Infos

Veröffentlichungen von F. X. Wortmann und D. Althaus hier als download!

 

Bücher:

Althaus D., Wortmann F.X.:
Stuttgarter Profilkatalog I
Vieweg Verlag, Braunschweig/Wiesbaden, ISBN 3-528-08464-2, 1981

Althaus,D.:
Auszug aus dem Stuttgarter Profilkatalog I
Institut für Aerodynamik und Gasdynamik, Stuttgart, 1996

Althaus D.:
Profilpolaren für den Modellflug
Neckar-Verlag VS-Villingen, ISBN 3-7883-0158-9, 1980

Althaus D.: 
Profilpolaren für den Modellflug, Band 2
Neckar-Verlag VS-Villingen, ISBN 3-7883-0134-1, 1985

Althaus D.: 
Niedriggeschwindigkeitsprofile (Stuttgarter Profilkatalog II)

Vieweg Verlag, Braunschweig/Wiesbaden, ISBN 3-528-03820-9, 1996

 

 

 

Veröffentlichungen seit 1993:

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Althaus D., Würz W.: 
Wind Tunnel Tests of the SM701 Airfoil and the UAG 88-143/20 Airfoil
Technical Soaring, Vol.17 No.1, pp21-32, 1993

Althaus D., Würz W.:
Experimental Investigation of Laminar Separation Bubbles
Gersten K. (Ed.), Physics of Separated Flows - Numerical, Experimental and Theoretical Aspects, NNFM, Vol.40, Vieweg-Verlag Braunschweig, 1993

Würz W.: 
Hitzdrahtmessungen zum laminar-turbulenten Strömungsumschlag in anliegenden Grenzschichten und Ablöseblasen sowie Vergleich mit der linearen Stabilitätstheorie und empirischen Umschlagskriterien
Dissertation, Universität Stuttgart, 1995

Würz W., Wagner S.: 
Experimentelle Untersuchungen zur Störungsanfachung in anliegenden Grenzschichten und Ablöseblasen
7.AG-STAB Workshop, DLR-Göttingen, 14.-16.11.1995

Krauter J.: 
Windkanaluntersuchungen am Rumpf-Flügelübergang eines Segelflugzeugs
 
19. Symposium für Segelflugzeugentwicklung, Braunschweig, 23.-24.11.1995

Würz W., Wagner S.: 
Experimentelle Untersuchungen zur Störungsanfachung in anliegenden Grenzschichten und Ablöseblasen
AG-STAB Jahresbericht 1995

Althaus D.: 
Niedriggeschwindigkeitsprofile

ISBN 3-528-03820, Vieweg Verlag Braunschweig/Wiesbaden 1996

Würz W., Wagner S.:
Experimentelle Untersuchungen zur Umschlagsentwicklung in anliegenden Grenzschichten und Ablöseblasen (2334kB)

10. DGLR/AG-STAB Fach-Symposium, Braunschweig, 11.-13.11.1996

Funk P., Würz W.:
Experimentelle Untersuchungen zur Widerstandsverminderung durch Riblets am Tragflügelprofil eines Segelflugzeugs der Standardklasse

10. Symposium für Segelflugzeugentwicklung, Stuttgart, 18.-19.11.1996

Würz W., Wagner S.: 
Experimental Investigations of Transition Development in Attached Boundary Layers and Laminar Separation Bubbles

Körner H., Hilbig R. (Eds.), New Results in Numerical and Experimental Fluid Mechanics, NNFM, Vol.60, Vieweg-Verlag Braunschweig, 1997

Würz W., Wagner S.: 
Hot-Wire Measurements and Transition Prediction in Boundary Layers with Adverse Pressure Gradient
Proceedings of the Colloquium on Fluid Dynamics `97, Prague 21.-23.10.1997

Würz W.:
Entwurf und Vermessung von 2 Profilen für Segelflugzeuge der Standardklasse (554kB)
Symposium für Segelflugzeugentwicklung 1997, Stuttgart, 11.-12.11.1997

Würz W., Herr S., Wagner S.: 
Experimentelle Untersuchung der Rezeptivität zweidimensionaler Grenzschichten
 
8. AG-STAB Workshop, Göttingen, 11.-13.11.1997

Wagner S., Würz W., Jäger G.: 
Experimentelle Untersuchung der Leitwerk-Propeller Kombination für das menschtragende Solarflugzeug Icaré 2
AG-STAB Jahresbericht 1997

Würz W., Herr S., Wagner S.: 
Experimentelle Untersuchung der Rezeptivität zweidimensionaler Grenzschichten
AG-STAB Jahresbericht 1997

Würz W., Herr S., Wagner S.: 
Experimental Investigation on Receptivity of two-dimensional Boundary Layers due to Surface Non-Uniformities
Proceedings of the Colloquium on Fluid Dynamics `98, Prague 20.-22.10.1998

Würz W., Herr S., Wagner S., Kachanov Y.S.: 
Experimentelle Untersuchungen zur akustischen Rezeptivität einer Einzelrauhigkeit in einer 2-dimensionalen Grenzschicht
11. DGLR/AG-STAB Fach-Symposium, Berlin, 10.-12.11.1998

Würz W., Herr S., Wagner S., Kachanov Y.S.: 
Experimental Investigations on 3D Acoustic Receptivity of a Laminar Boundary Layer in the Presence of Surface Non-Uniformities(547kB)
Nitsche W., Heinemann H.J., Hilbig R. (Eds.), New Results in Numerical and Experimental Fluid Mechanics II, NNFM, Vol.72, Vieweg-Verlag Wiesbaden, 1999

Eppler R., Würz W.: 
Design Philosophies for Sailplane Airfoils with Flaps
OSTIV-Congress, Bayreuth, 6.8.-10.8.1999

Würz W., Herr S., Wörner A., Rist U., Kachanov Y.S.: 
3D acoustic receptivity of boundary layer on an airfoil in presence of localized surface non-uniformities. Experiment and DNS
In: Actual Problems of Physical Hydroaerodynamics. [Transactions of International Workshop "Outcomes and Perspectives of Cooperation of the European and Siberian Scientists in Field of Physical Hydromechanics" (Part I) and of International Conference on Stability and Turbulence of Homogeneous and Heterogeneous Flows (Part II)], pp. 1-64 - 1-65. Novosibirsk: Institute of Thermophysics, 1999

Ab 2000:

Würz W., Herr S., Wörner A., Rist U., Wagner S., Kachanov Y.S.:
Study of 3D Wall Roughness Acoustic Receptivity on an Airfoil (472kB)

Fasel H., Saric W. (Eds.), Laminar-Turbulent Transition, proc. of the IUTAM Symposium Sedona, Az./USA, September 13-17, 1999, pp. 91-96, Springer Verlag Berlin, 2000

Herr S., Würz W., Wagner S.: 
Experimentelle Untersuchungen zur akustischen Rezeptivität einer 2-dimensionalen Grenzschicht unter dem Einfluß eines Druckgradienten
9. AG-STAB Workshop, Göttingen, 9.-11.11.1999

Herr S.: 
Entwurf eines Profils mit frequenzselektivem Turbulator
Tragflügelseminar 1999/2000, Stuttgart, 17.02.2000

* Lutz Th., Würz W., Wagner S.:
Numerical Optimization and Wind-Tunnel Testing of Low Reynolds-Number Airfoils (317kB)
Conference on Fixed, Flapping and Rotary Wing Vehicles at very Low Reynolds Numbers, Notre Dame, Indiana, 5.-7.6.2000

Würz W., Herr S., Wörner A., Rist U., Wagner S., Kachanov Y.S.:
Experimental and Numerical Investigation of 3D Acoustic Receptivity due to Localized Wall Roughness (186kB)

ICMAR 2000, Novosibirsk, 9.-15.7.2000

Herr S., Würz W., Wörner A., Rist U., Wagner S., Kachanov Y.S.: 
Experimental and Numerical Investigation of 3D Wall Roughness Acoustic Receptivity on an Airfoil
ICTAM 2000, Chicago, 27.8.-2.9.2000

* Wörner A., Rist U., Herr S., Würz W., Wagner S., Kachanov Y.S.: 
Study of the Acoustic Receptivity of a Blasius Boundary Layer in the Presence of a Surface Non-Uniformity (485kB)
ECCOMAS 2000, Barcelona, 11.-14.9.2000

* Lang M., Marxen O., Rist U., Wagner S., Würz W.: 
LDA-Messungen zur Transition in einer laminaren Ablöseblase; Lasermethoden in der Strömungsmeßtechnik (261kB)
8. Fachtagung der Gala, Freising-Weihenstephan,12.-14.9.2000

Herr S., Wörner A., Würz W., Rist U., Wagner S.:
Experimentelle/Numerische Untersuchung zum Einfluss des Druckgradienten auf die akustische Rezeptivität einer Einzelrauhigkeit in einer 2-dimensionalen Profilgrenzschicht

12. DGLR/AG-STAB Fach-Symposium Stuttgart, 15.-17.11.2000

Herr S., Wörner A., Würz W., Rist U., Wagner S.:
Experimental/Numerical Investigation of the Influence of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of a 2D Airfoil (716kB)

Wagner S., Rist U., Heinemann H.J., Hilbig R. (Eds.), New Results in Numerical and Experimental Fluid Mechanics III, NNFM, Vol.77, Springer-Verlag Berlin, 2002

Würz W.:
Rezeptivität und Transition, Grundlagenuntersuchungen am Laminarwindkanal (1497kB)
24. Segelflugsymposium, Stuttgart, 20.u.21.11.2000

Friedrichs C.:
Eyecatcher im Test - Steuerbügel im Windkanal (1303kB)
Fly and Glide, 2/2001, S.55-59

Ivanov A.V., Würz W., Herr S., Wagner S.: 
Experimental Investigation of 3-D Acoustic Receptivity due to a Surface Vibration on an Airfoil
EUROMECH Colloquium 423 'Boundary-Layer Transition in Aerodynamics‘, Stuttgart, 2.-4.4.2001

Herr S., Würz W., Wagner S.:
Experimentelle Untersuchungen zur Charakterisierung des dominanten Störspektrums in der Anströmung anhand der Rezeptivität einer Oberflächenstörung an einem 2-dimensionalen Tragflügelprofil
10. AG STAB-Workshop, Göttingen, 14.-15.November 2001

* Lang M., Rist U., Wagner S., Würz W.:
Überblick über aktuelle Untersuchungen zur Transition in einer laminaren Ablöseblase am IAG
26. Segelflugsymposium, Braunschweig, 21.-22.11.2001

* Lutz Th., Würz W., Wagner S.:
Numerical Optimization and Wind-Tunnel Testing of Low Reynolds Number Airfoils
Thomas J. Mueller (ed.): Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, Vol. 195, AIAA 2001

Würz W., Herr S., Wagner S., Kachanov Y.S.:
A First Experimental Approach to the Distributed 3D-Vortex Receptivity of a Boundary Layer on an Airfoil (1533kB)
ICMAR 2002, Novosibirsk, 1.-7.7.2002

Ivanov A.V., Würz W., Herr S., Wagner S., Kachanov Y.S.:
Experimental Study of Essentially Non-Stationary Acoustic Receptivity of a Boundary Layer on an Airfoil due to Surface Non-Uniformities (268kB)
ICMAR 2002, Novosibirsk, 1.-7.7.2002

Sartorius D.:
Grenzschichtuntersuchungen im Bereich kleiner Reynolds-Zahlen an laminaren Ablöseblasen in der Nähe der Profilendkante
DGLR-Jahrestagung 2002, Stuttgart, 21.-24.9.2002

Herr S., Würz W., Wagner S.:
Experimentelle Untersuchungen zur wirbelbehafteten Rezeptivität einer Oberflächenstörung an einem 2-dimensionalen Tragflügelprofil

13.DGLR/AG-STAB Fach-Symposium München, 12.-14.11.2002

Sartorius D., Würz W., Wagner S.:
Experimentelle Untersuchung zur Kontrolle laminarer Ablöseblasen
26. Segelflugsymposium, Stuttgart, 21.u.23.11.2002

Feßler R., Würz W.:
Flugerprobung eines Funk-Umschlagsensors
Folien des Vortrags (296kB)
            Beschreibung des Sensors
26. Segelflugsymposium, Stuttgart, 21.u.23.11.2002

Würz W., Herr S., Wörner A., Rist U., Wagner S., Kachanov Y.S.:
Three-Dimensional Roughness-Acoustic Receptivity of a Boundary Layer on an Airfoil. Experiment and DNS
Journal of Fluid Mechanics, Vol. 478, pp. 135-163, 2003

Herr S., Würz W., Wörner A., Rist U., Wagner S., Ivanov A., Kachanov Y.S.:
Systematic investigations of 3D acoustic receptivity with respect to steady and unsteady disturbances. Experiment and DNS
Wagner S., Kloker M., Rist U.(Eds.), Recent Results in Laminar-Turbulent Transition - Selected Numerical and Experimental Contributions from the DFG-Verbundschwerpunktprogramm "Transition" in Germany, NNFM, Vol.86, pp.75-90, Springer-Verlag Berlin, 2003

Herr S., Würz W., Wagner S.:
Experimental investigation of local vortex roughness receptivity of a boundary layer on 
an airfoil
Breitsamer C., Laschka B., Heinemann H.(Eds.), New Results in Numerical and Experimental 
Fluid Mechanics IV, NNFM, Vol.87, pp.148-155, Springer-Verlag Berlin, 2004

Sartorius D., Würz W., Wagner S.:
Auslegung eines Membranaktuators unter Berücksichtigung der Stabilitäts- und Rezeptivitätseigenschaften der Grenzschicht
11. AG STAB-Workshop, Göttingen, 4.-5.November 2003

* Guidati S., Herrig A., Ostertag J., Würz W., Wagner S.:
Numerical Simulation and Measurement of Boundary-Layer Induced Noise on Wing Sections
4th Aeroacoustics Workshop, Aachen, 26.-27. Februar 2004

Würz W.
A Coherent Particle Velocity Method for Measurement of Trailing Edge Noise on Airfoils
Fluid Dynamics Research - Selected Recent Results, An International colloquium on the occasion of the retirement of Prof. Dr.-Ing. Siegfried Wagner, Stuttgart, 7.Mai 2004

Würz W., Sartorius D., Wagner S., Borodulin V.I., Kachanov Y.S.
Experimental study of weakly nonlinear interactions of instability waves in a non self-similar boundary layer on an airfoil
Part I: Base flow and initially tuned resonances

ICMAR 2004, Novosibirsk, 28.6.-2.7.2004

Sartorius D., Würz W., Wagner S., Borodulin V.I., Kachanov Y.S.:
Experimental study of weakly nonlinear interactions of instability waves in a non self-similar boundary layer on an airfoil, Part II: Influence of frequency and spanwise-wavenumber detunings
ICMAR 2004, Novosibirsk, 28.6.-2.7.2004

Würz W., Guidati S., Herrig A., Lutz Th., Wagner S.
Measurement of trailing edge noise by a coherent particle velocity method
ICMAR 2004, Novosibirsk, 28.6.-2.7.2004

Sartorius D., Würz W.,  Wagner S., Borodulin V.I., Kachanov Y.S.
Resonant Interactions of 3D Instability Waves in an Airfoil Boundary Layer for Harmonic and Broadband Perturbations
XXI. International Congress of Theoretical and Applied Mechanics (ICTAM), Warsaw, 15.-21.8.2004

* Lutz Th., Würz W.,  Herrig A., Braun K.,  Wagner S.
Numerical Optimization of Silent Airfoil Sections
DEWEK 2004, 7th German wind energy conference, Wilhelmshaven, 20.-21.10.04

Sartorius D., Würz W., Ries T., Kloker M.,  Wagner S., Borodulin V.I., Kachanov Y.S.
Experimental study of resonant interactions of instability waves in an airfoil boundary layer
Sixth IUTAM Symposium on Laminar-Turbulent Transition, Bangalore, 13.-17.12.04
Fluid Mech. and its Applications, Vol.78, Rama Govindarajan (Ed.), pp. 159-165, Springer Verlag Berlin, 2006

Ab 2005:

Herrig A.
Development of aeroacoustic measurement methods for noisy aerodynamic wind tunnels
EAWE PhD Seminar, Athen, 22.-23. September 2005

Herrig A.,  Würz W., Lutz Th., Braun K., Krämer E., Oerlemans S.
Trailing Edge Noise Measurements of Wind Turbine Airfoils in Open and Closed Test Section Wind Tunnels
First International Meeting on Wind Turbine Noise: Perspectives for Control, Berlin, 17.-18.October 2005

* Lutz Th., Herrig A.,  Würz W.,  Braun K., Krämer E.
Constrained Aerodynamic & Aeroacoustic Design of Wind-Rotor Airfoils
First International Meeting on Wind Turbine Noise: Perspectives for Control, Berlin, 17.-18.October 2005

* Schepers J.G., Curvers T., Oerlemans S., Braun K., Lutz Th., Herrig A., Würz W.,  Mendez Lopez B.
Sirocco: Silent Rotors by Acoustic Optimation
First International Meeting on Wind Turbine Noise: Perspectives for Control, Berlin, 17.-18.October 2005

Sartorius D., Würz W.,  Wagner S., Borodulin V.I., Kachanov Y.S.
Experimental investigation of weakly nonlinear interactions of instability waves in an airfoil boundary layer
AG STAB Mitteilung 2005

Würz W.,  Herrig A., Krämer E.
Messung von Hinterkantenlärm an Tragflügelprofilen mit einer "Coherent Particle Velocity"-Methode
AG STAB Mitteilung 2005

Ivanov A.V., Würz W., Herr S., Wagner S., Kachanov Y.S.
Experimental investigation of 3D acoustic receptivity of an airfoil boundary layer due to surface vibrations
European Journal of Mechanics B/Fluids 24 (2005) 621-641

Würz W., Sartorius D., Kloker M., Ries T., Wagner S., Smorodsky B., Borodulin V.I., Kachanov Y.S.
Experimental, numerical and theoretical investigation of weakly nonlinear stages of transition in a non self-similar boundary layer
12. AG STAB-Workshop, Göttingen, 8.-9.November 2005

Herrig A., Würz W., Krämer E.
Akustisches Messverfahren für den Einsatz in Windkanälen mit hohem Hintergrundstörpegel
12. AG STAB-Workshop, Göttingen, 8.-9.November 2005

de Paula I.B.,  de Medeiros M.A.F., Würz W., Mendonça M.T.
Fundamental resonance induced by a 3D shallow roughness
58th Annual Meeting of the Division of Fluid Mechanics, American Physical Society, Chicago, 20.-22. November 2005

* Schepers J.G., Curvers T., Oerlemans S., Braun K., Lutz Th., Herrig A., Würz W.,  Mendez Lopez B.,
Arelt R., Maeder T.
Sirocco: Silent Rotors by Acoustic Optimation
European WInd Energy Conference, Athen, 27.2.-2.3.2006

Herrig A., Würz W., Lutz Th., Krämer E.
Trailing-Edge Noise Measurements Using a Hot-Wire Based Coherent Particle Velocity Method
24th AIAA Applied Aerodynamics Conference, San Francisco, 5.-8. June 2006

* Lutz Th., Herrig A., Würz W., Kamruzzaman M., Krämer E.
Design and Wind-Tunnel Verification of Low-Noise Airfoils for Wind Turbines
24th AIAA Applied Aerodynamics Conference, San Francisco, 5.-8. June 2006

De Paula I. B., Medeiros M. A. F., Würz W., Mendonça M. T. Experimental study on the boundary layer transition induced by a shallow 3D roughness element
6th Euromech Fluid Mechanics Conference, Stockholm, 26-30 June 2006

*Lutz Th., Würz W., Herrig A., Braun K., Krämer E., Schepers J.G., Curvers A.P.W.M., Oerlemans S., Matesanz A., Ahrelt R., Maeder T., Herr S.
New Results from the European SIROCCO Project: Silent Rotors by Acoustic Optimization
DEWEK 2006, 8th German Wind Energy Conference, Bremen, 22.-23. November 2006

Kobiela B., Lerch A., Herrig A., Würz W.
Grenz-N-Faktor Betimmung bei Reynoldszahlen<600.000 - Ein neuer Ansatz für Kombinierte Freiflug- und Windkanalmessungen
Segelflug-Symposium, Darmstadt, 23.-24. November 2006

Herrig A., Würz W., Lutz Th., Krämer E., Wagner S.
Trailing-Edge Noise Measurements of a NACA 0012 Airfoil using the Coherent Particle Velocity Method
Int. Conference on Methods of Aerophysical Research ICMAR, 05.-10.Feb. 2007

Herrig A., Würz W., Lutz Th., Krämer E., Wagner S.
Measurement of Airfoil Trailing Edge Noise with the Coherent Particle Velocity Method
33rd German Annual Conference on Acoustic (DAGA), Stuttgart, 19.-22.März 2007

*  Lutz Th., Herrig A., Würz W., Kamruzzaman M., Krämer E.:
Design and Wind-Tunnel Verification of Low-Noise Airfoils for Wind Turbines
AIAA Journal, Vol. 45, No. 4, April 2007

* Schepers J.G., Curvers T., Oerlemans S., Braun K.,  Lutz Th.,  Herrig A., Würz W.,  Matesanz A.,
Fisher M.,  Koegler K.,  Maeder T.
Sirocco: Silent Rotors by Acoustic Optimisation
Second International Meeting on Wind Turbine Noise, Lyon, 20.-21.September 2007

Miller A.,Müller M., Neumann S.O., Würz W.
Numerische Untersuchung der aerodynamischen Kräfte an einem Flügelelement mit unterbrochenem Hinterkantenschlitz
ANSYS Conference & 25th CADFEM Users' Meeting 2007, Dresden, 21.-23. November 2007

Herrig A., Würz W., Krämer E., Wagner S.
Hitzdraht-basierte Messungen von Hinterkantenlärm an NACA-0012-Profilen
AG STAB Workshop, Göttingen, 14.-15. Nov.2007

De Paula I.B., Würz W., Medeiros M.A.F.
Experimental Study of a Tollmien-Schlichting wave interacting with a shallow 3-D roughness element
Journal of Turbulence Volume 9 N 7 (2008) pp.1-23
Herrig A., Würz W., Krämer E., Wagner S.
New CPV-Results of NACA 0012 Trailing-Edge Noise
Int. Conference on Methods of Aerophysical Research ICMAR , 30.June-06.July 2008

De Paula I.B., Sartorius D., Krämer E., Kachanov Y.S.
Experimental Study of Broadband Resonant Interactions in an Non-Self Similar Boundary Layer of an Airfoil
Int. Conference on Methods of Aerophysical Research ICMAR , 30.June-06.July 2008
Herrig A., Würz W., Krämer E., Wagner S.
Trailing-Edge Noise Measurements on NACA 0012 Airfoils Using the 
Coherent Particle Velocity Method
15th International Congress of Sound and Vibration, Daejon, Korea, 06.-10.07. 2008
Würz W., Sartorius D., Kloker M., Wagner S., Smorodsky B., Borodulin V.I., Kachanov Y.S.
Weakly nonlinear stages of transition in an airfoil boundary layer. A combined experimental, numerical 
and theoretical investigation
Deutscher Luft- und Raumfahrtkongress der DGLR, Darmstadt, 23.-25.09. 2008
* Schreyer A.-M., Würz W., Krämer E., Talamelli A., Alfredsson H.
Experimental Flow Studies on Separation and Reattachment in the Vicinity of Sharp, Wedge Shaped 
Leading Edges at Low Reynolds Numbers
16. DGLR-Fachsymposium der STAB, Aachen, 03.-04.11.2008
Herrig A., Würz W.
Untersuchungen zur atmosphärischen Turbulenz in Bodennähe
32. Symposium für Segelflugzeugentwicklung, Gersfeld, 20.-21.11.2008
Käser, K., Ruppert R., Würz W.
Untersuchungen zur Aerodynamik bespannter Tragflügel am Beispiel des Archaeopteryx
32. Symposium für Segelflugzeugentwicklung, Gersfeld, 20.-21.11.2008
Cerretelli C., Gharaibah E., Toplack G., Gupta A., Würz W.
Unsteady Separation Control for Wind Turbine Applications at Full Scale Reynolds Number
47th AIAA Aerospace Sciences Meeting, AIAA 2009-380, Orlando, 5.-8.01. 2009
* Kamruzzaman M., Lutz Th., Ivanov A., Herrig A., Würz W., Krämer E.:
Evaluation of Measured Anisotropic Turbulence Two-point Correlation Data for the Accurate Prediction 
of the Turbulence Noise Sources 
AIAA Paper, 2009-3313-818, 15th AIAA/CEAS Aeroacoustics Conference, Miami, USA, 11.-13.05.2009 
* Kamruzzaman M., Lutz Th., Herrig A., Krämer E.:
Semi-empirical Modeling of Turbulent Anisotropy for Airfoil Self Noise Prediction
AIAA Journal, 50(1): 46-60, January, 2012, DOI: 10.2514/1.56982.
Old version in Proc. of 16th AIAA/CEAS Aeroacoustics Conference, 7-8 June, 2010, Sweden, AIAA-2010-3878 
* Kamruzzaman M. , Herrig A., Lutz Th., Würz W., Krämer E., Wagner S.:
Comprehensive Evaluation and Assessment of Trailing Edge Noise Prediction Based on Dedicated Measurements 
Noise Control Engineering Journal, 59(1):54-67, Jan-Feb., 2011. Also presented in Wind Turbine Noise-2009,
Aalborg, Denmark, 17.-19.06.2009
de Paula  I. B., Würz W., Krämer E., Borodulin V. I., Kachanov Y. S.
Experimental study of resonant interaction of modulated waves in a non self-similar boundary layer
7th IUTAM Symposium on Laminar-Turbulent Transition, KTH Stockholm. 22.-26.06.2009
de Paula I. B., Würz W., Medeiros M. A. F.
Effect of a single three-dimensional roughness element on the boundary layer transition
7th IUTAM Symposium on Laminar-Turbulent Transition, KTH Stockholm. 22.-26.06.2009
de Paula  I. B., Würz W., Krämer E., Borodulin V. I., Kachanov Y. S.
Experimental investigation of weakly nonlinear interaction of Tollmien-Schlichting waves in a 
non self-similar boundary layer.
AG STAB Workshop, Göttingen, 11.-12.11.2009
Ab 2010:
de Paula  I. B., Würz W., Krämer E., Borodulin V. I., Kachanov Y. S.
Production of Seeds for Subharmonic Resonance in the Evolution of Modulated TS-Waves 
on an Airfoil Boundary Layer
8th Euromech Fluid Mechanics Conference, Bad Reichenhall, 13.-16.09.2010
de Paula  I. B., Würz W., Krämer E., Borodulin V. I., Kachanov Y. S.
Generation of seeds for subharmonic resonance in an airfoil boundary-layer transition initiated 
by modulated TS waves
Int. Conference on Methods of Aerophysical Research - ICMAR, Novosibirsk, Russia, 01.-06.11.2010
* Kamruzzaman M., Bekiropoulos D., Wolf A., Lutz Th., Würz W., Krämer E.:
Study of Turbulent Boundary Layer Wall Pressure Fluctuations Spectrum Models for Trailing-edge Noise Prediction
Proc. of 15th Int. Conf. on the Methods of Aerophysical Research (ICMAR 2010), 
Akademgorodok, Novosibirsk, Russia, 01.-06.11.2010
de Paula  I. B., Würz W., Krämer E., Borodulin V. I., Kachanov Y. S.
Introduction of initial seeds for subharmonic resonance by modulation of T-S waves in an airfoil boundary layer
17. DGLR-Fach Symposium der STAB, Berlin, 09.-10.11.2010
* Wolf A., Lutz Th., Würz W.,  Stalnov O. and Krämer E.:
Impact of Suction on Boundary-Layer and Noise Emission of Wind Turbine airfoils
DEWEK-2010, Bremen, 17.-18.11.2010
* Wolf A., Lutz Th.,  Würz W.,  Stalnov O. and  Seifert A.:
Trailing edge noise reduction of wind turbine airfoils by active flow control
Proceedings of Fourth International Meeting on Wind Turbine Noise, Rome, Italy,12.-14.04.2011
* Kamruzzaman M.,  Lutz Th.,  Würz W. and Krämer  E.:
On the Length Scales of Turbulence for Aeroacoustic Applications
AIAA Paper No. 2011-2734. Proceedings of 17th AIAA/CEAS Aeroacoustics Conference, 
Portland, Oregon, USA, 06.-08.06.2011
* Kamruzzaman M., Lutz Th., Würz W. , Shen W., Zhu W., Hansen M. O. L., Bertagnolio F., Madsen H. Aa. :
Validations and Improvements of Airfoil Trailing-edge Noise Prediction Models Using Detailed Experimental Data
published in online at Wind Energy, DOI: 10.1002/we.505, November 2011
Plogmann B., Würz W., Krämer E.:
Interaction of a 3D roughness element with a laminar boundary layer near an airfoil leading edge
AG STAB Workshop, Göttingen, 09.-10.11.2011

Würz W., Sartorius D., Kloker M., Borodulin V. I., Kachanov Y. S., Smorodsky B.V.
Nonlinear instabilities of a non-self-similar boundary layer on an airfoil: experiments, DNS, and theory
European Journal of Mechanics / B Fluids 31(2012)102-128

Herrig A., Kamruzzaman M., Würz W., Wagner S.:
Broadband Airfoil Trailing-edge Noise Prediction from Measured Surface Pressures and Spanwise Length Scales
Int. Journal of Aeroacoustics 12, No.1+2, pp.53-82 (2013)

Plogmann B., Würz W., Krämer E.:
Interaction of a Laminar Boundary Layer with a Cylindrical Roughness Element near an Airfoil Leading Edge
AIAA Paper 2012-3077, 42nd AIAA Fluid Dynamics Conference and Exhibit,
New Orleans, Louisiana, June 25-28, 2012

Würz W., Sartorius D., Kloker M., Borodulin V. I., Kachanov Y. S., Smorodsky B.V.:
Detuned resonances of Tollmien-Schlichting waves in an airfoil boundary layer: Experiment, theory, and direct numerical simulation
Phys. Fluids 24, 094103 (2012)
 

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