|
|
|
|
|
Álvaro Muñoz and Pablo García-Fogeda
This paper compares various procedures for determining the optimal control law for a wing section in compressible flow. The flow regime includes subsonic, sonic and supersonic flows. For the evolution of the system in the Laplace plane, the present metho...
ver más
|
|
|
|
|
|
|
|
|
|
|
Álvaro Muñoz and Pablo García-Fogeda
In this paper, a unified method for the computation of the unsteady aerodynamic forces in the Laplace domain for a wing section in subsonic, sonic and supersonic potential flows is presented. The subsonic solution is a new development based on the pressu...
ver más
|
|
|
|
|
|
|
|
|
|
|
Aykut Tamer, Vincenzo Muscarello, Giuseppe Quaranta and Pierangelo Masarati
Helicopter Emergency and Medical Service (HEMS) vehicles require a specially configured cabin that supports the quick transport of a rescue team to the site of an emergency and return of patients back to a full capacity hospital, while sustaining the pat...
ver más
|
|
|
|
|
|
|
|
|
|
|
David Quero, Pierre Vuillemin and Charles Poussot-Vassal
In this work, a new approach for the generation of a generalized state-space aeroservoelastic model based on tangential interpolation is presented. The resulting system of differential algebraic equations (DAE) is reduced to a set of ordinary differentia...
ver más
|
|
|
|
|
|
|
|
|
|
|
D.E. Biskri, R.M. Botez, N. Stathopoulos, S. Thérien, M. Dickinson, and A. Rathe
Pág. 1217 - 1230
|
|
|
|
|
|