Rotary Derivatives in Yaw: Calculation by Lifting Plane Theory of the Rolling and Yawing Moments of a Wing Due to Rotary Motion in Yaw

Author: A.M.I.Mech.E. V.M. Falkner   B.Sc.  

Publisher: Emerald Group Publishing Ltd

ISSN: 0002-2667

Source: Aircraft Engineering, Vol.23, Iss.2, 1993-12, pp. : 44-54

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract