Theory of the oscillating wing with aerodynamically balanced control surface in a two-dimensional, subsonic, compressible flow
By: R. Timman and Adriaan Isak Van de Vooren.
Contributors: Van de Vooren, Adriaan Isak.; National Aeronautical Research Institute (Netherlands)
Series: National Aeronautical Research Institute. Report -- F. 54
Publisher: Nationaal Luchtvaartlaboratorium
Published: 1949
Place of publication: Amsterdam
Number of pages: 54
Notes: Bibliographical references: p. 37-38.