Investigation of the response to random wind gusts of a typical subsonic fighter aircraft in level flight with Mach number 0.9 at sea level
By: K. Flodin and M. Sundstrom.
Contributors: Sundstrom, M.; Royal Institute of Technology (Sweden). Dept. of Aeronautical Engineering
Publisher: Royal Institute of Technology, Dept. of Aeronautical Engineering
Published: 1958
Place of publication: Stockholm
Notes: 25 p. : ill.

Contract number: Bibliographical references: p.9