An Improved Method to Calculate the Nonlinear Rolling Moment Due to Differential Fin Deflection of Canard Controlled Missiles
AIAA Atmospheric Flight Mechanics Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Approximate Method to Calculate Nonlinear Rolling Moment due to Differential Fin Deflection
Online Contents | 2012
|An Approximate Method to Calculate Nonlinear Rolling Moment Due to Differential Fin Deflection
British Library Conference Proceedings | 2012
|