An approximate method for determining the incompressible, irrotational flow around a symmetrical wing section
Series: K[ungl.] T[ekniska] H[ögskolan] AERO T[echnical] N[ote] -- no. 7
Publisher: Division of Aeronautics, Royal Institute of Technology
Published: 1949
Place of publication: Stockholm
Language: eng
Number of pages: 18
Notes: Bibliography: p. 7.