An Improved Method to Calculate the Nonlinear Rolling Moment Due to Differential Fin Deflection of Canard Controlled Missiles (AIAA 2015-1018)
AIAA atmospheric flight mechanics (Conference)
01.01.2015
21 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
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
|