An investigation on vertical tailplane contribution to aircraft sideforce

Author:

Nicolosi Fabrizio,Della Vecchia Pierluigi,Ciliberti Danilo

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Computational Fluid Dynamics: The Basics with Applications;Anderson,1995

2. Alexandre P. Antunes, Ricardo Galdino da Silva, João Luiz, F. Azevedo, On the effects of turbulence modeling and grid refinement on high lift configuration aerodynamic simulations, in: 28th ICAS (International Council of Aeronautics and Astronautics) Conference, 23–28 September 2012, ISBN 9780956533319.

3. R.J. Bamber, R.O. House, Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. II – Rectangular NACA 23012 wing with a circular fuselage and a fin, TN-730, National Advisory Committee for Aeronautics, 1939.

4. Jack D. Brewer, Jacob H. Lichtenstein, Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45° sweptback wing and tail surfaces, Technical Note 2010, National Advisory Committee for Aeronautics, 1950.

5. Franklin W. Diederich, A plan-form parameter for correlating certain aerodynamic characteristics of swept wings, TN-2335, National Advisory Committee for Aeronautics, 1951.

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