IMP PAN - Department of Transonic Flows & Numerical Methods

Participation in European Union grants:

In the past - IV Framework:

EUROSHOCK I and II (1994-1999,DLR) - shock wave boundary layer interaction and its passive and active control

Past - V Framework:

AITEB (1999-2003, Rolls-Royce) - gas turbine cooling

INCO-2 (2000, IMP PAN) - large conference support

HELIX (2001-2003, Airbus) - subcontract (Institute of Aviation, Warsaw)

Current - VI Framework:

UFAST project (2006- ), UFAST Homepage) - IMP PAN is a Coordinator of Unsteady eFfects of shock wAve induced SeparaTion Project.
UFAST project is to foster experimental and theoretical work in the highly non-linear area of unsteady shock wave boundary layer interaction (SWBLI).


Prof. Piotr DOERFFER ul. Fiszera 14 PL-80 952 Gdansk, POLAND fax: (+48) 58 341 61 44 e-mail:doerffer@imp.gda.pl


Shock wave configuration at triple point at low Mach number	Flow control for noise and drag reduction	Gas turbine cooling (AITEB)

16 Sept 2003 ::: Main page finished

After struggling with computer problems (burned motherboard) I managed to finish the content of main page. It's obvious that links not working yet, but will be a.s.a.p.

21 Sept 2003 ::: Page uploaded

The webpage has been uploaded to our WWW server. Please note that we are still working on it. Currently only main page and Transonic Wind Tunnel subsection has been finished.

13 Oct 2003 ::: Page getting functional

Now we're on the right way to finish. We had just added he "Staff" & "Numerical Tools" sections. Also the "Thematic interests" section has been partially completed.

Main Staff Transonic Wind Tunnel Numerical Tools Thematic Interests Cooperation