1. Sobieczky, H.: Computational Methods for the Design of Adaptive Airfoils and Wings. Notes on Numerical Fluid Mechanics, Vol. 2, ed. E. H. Hirschel, Vieweg (1979) pp. 269–278.
2. Sobieczky, H.: DFVLR-F5 Test Wing Configuration for Computational and Experimenta Experimental Aerodynamics, Wing Surface Generator Code, Control Surface and Boundary Conditions. Notes on Num. Fluid Mechanics, Vol. 22, ed. W. Kordulla, Vieweg (1988), pp. 27–37.
3. Sobieczky, H., Hefer, G., Tusche, S.: DFVLR-F5 Test Wing Experiment for Computational Aerodynamics. AIAA 5. Appl. Aerodynamics Conf. Proc., AIAA 87–2485CP, (1987), Notes on Numerical Fluid Mechanics, Vol. 22, ed. W. Kordulla, Vieweg, (1988), pp.4 – 22.
4. Sobieczky, H.: Aircraft Surface Generation. Results of EC Brite/Euram Project ‘Euromesh’ 1990–92, Notes on Numerical Fluid Mechanics, Vol. 44, ed. N. Weatherill et al, Vieweg (1993), pp. 71–76.
5. Sobieczky, H.: Geometry Generator for CFD and Applied Aerodynamics, in: New Design Concepts for High Speed Air Transport. CISM Courses and Lectures No. 366, Springer (Wien, New York), (1997) pp 137–157.