Experimental determination of the aerodynamic coefficients of an oscillating wing in incompressible, two-dimensional flow. Part III
Subtitle: Experiments at zero airspeed
By: H. Bergh.
Contributors: National Aeronautical Research Institute (Netherlands)
Series: National Aeronautical Research Institute. Report -- F. 103
Publisher: Nationaal Luchtvaartlaboratorium
Published: 1952
Place of publication: Amsterdam
Notes: Bibliographical references: p. 5-6.