dr inż. Andrzej Krzysiak

Scientific interests:

Applied aerodynamics.

Most important publications:

  1. Krzysiak A. (2013). Improvement of helicopter performance using self-supplying air jet vortex generators. Journal of Kones 2013. Vol. 20. No. 2. ISNN 1231-4005.
  2. Krzysiak A. (2011). Zastosowanie nowego rodzaju strumieniowych generatorów wirów do sterowania przepływem. Prace Instytutu Lotnictwa. Zeszyt 212, Warszawa, ISSN 0509-6669.
  3. Krzysiak A. (2008). Control of Flow Using Self-Supplying Air Jet Vortex Generators. AIAA Journal. Vol. 46. No. 9, pp. 2229-2234, ISSN 0001-1452.
  4. Krzysiak A., Narkiewicz J. (2006). Aerodynamic Loads on Airfoil with Trailing-Edge Flap Pitching with Different Frequencies. Journal of Aircraft. Vol. 43, No. 2, pp. 407-418, ISSN 0021-8669.
  5. Krzysiak A. (2006). Experimental Investigation of a Dynamic Stall on the Oscillating NACA 0012 Airfoil. Transactions of the Institute of Aviation 187. Warsaw, ISSN 0509-6669.


  1. Multi-level Embedded Closed-Loop Control System for Fluidic Active Flow Control – ESTERA. European project carried out in 2011-2013 within the CLEAN SKY platform. Project coordinator.
  2. Basic wind tunnel investigation to explore the use of Active Flow Control technology for aerodynamic load control – STARLET. European project carried out in 2012-2014 within the CLEAN SKY platform.  Experimental research manager.
  3. Advanced, light glider with an innovative wing structure. Project executed in 2013-2015 under OP IE 1.3.1 No. OP IE 01/03/01-14-087/12. Experimental research manager.
  4. Modernisation of the tunnel power transmission system Æ 5m. Project executed in 2012-2015, financed by the Ministry of Science and Higher Education. Project Manager in the years 2012 -2013.
  5.  Unsteady effect of shock wave induced separation – UFAST. European project carried out in 2006-2009. Experimental research contractor.
  6. Development and implementation of a new generation of technological and material structural solutions for a rotor and airframe components of the PZL W-3A Sokół helicopter. Project executed in 2007-2010, financed by the Ministry of Science and Higher Education. Experimental research contractor.
  7. Design and construction of the IRYDA training-combat aircraft. Project carried out in 1980-1997. Experimental research contractor.


  1. W. Stalewski, A. Krzysiak, M. Schuller. Application for European patent (dated 10/06/2014) No. 14460033-EP14460033 “Autonomous Active Flow Control System.”
  2. A. Krzysiak. Application for Patent No. P394222 (dated 15/03/2011). Supplementary application to P.380813 “Segment of aerodynamic profile with jet vortex generators.” Patent Office of the Republic of Poland, Warsaw 2011.
  3. A. Krzysiak. Patent No. 206221 Segment of aerodynamic profile with jet vortex generators.”  Patent Office of the Republic of Poland, Warsaw 2010.
  4. A. Krzysiak. Patent No. 196759 “System forcing independent oscillating motion of the model of the profile and its flap in a wind tunnel.” Patent Office of the Republic of Poland, Warsaw 2008.

List of awards and decorations:

  1. Medal for Long Service – 1st degree, Warsaw, 2011; Award of the President of the Republic of Poland.
  2. Awards for the best research work in the years: 1991, 2001, 2007, 2008 and 2010. Awards conferred by the Director of the Institute of Aviation.