Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow
By: E. M. De Jager.
Contributors: National Aeronautical Research Institute (The Netherlands)
Series: National Aeronautical Research Institute. Report -- F. 155
Publisher: National Aeronautical Research Institute
Published: 1954
Place of publication: Amsterdam
Number of pages: 21
Subjects: Ailerons
Notes: Prepared for Reports and Transactions, Vol XIX.