Advances in Aircraft and Spacecraft Science

CONTENTS

Volume 5, Number 1, 2018

• A WFE and hybrid FE/WFE technique for the forced response of stiffened cylinders

  Fabrizio Errico, M. Ichchou, S. De Rosa, O. Bareille and F. Franco

  Abstract | Full Text (1K)

  pages 1-19.

  DOI: 10.12989/aas.2018.5.1.001

• Geometrical nonlinear bending characteristics of SWCNTRC doubly curved shell panels

  Shivaji G. Chavan and Achchhe Lal

  Abstract | Full Text (2K)

  pages 021-49.

  DOI: 10.12989/aas.2018.5.1.021

• Dynamic calculation of a tapered shaft rotor made of composite material

  Zahi Rachid, Refassi Kaddour and Habib Achache

  Abstract | Full Text (2K)

  pages 051-71.

  DOI: 10.12989/aas.2018.5.1.051

• Constant speed, variable ascension rate, helical trajectories for airplanes

  Gilles Labonte

  Abstract | Full Text (2K)

  pages 073-105.

  DOI: 10.12989/aas.2018.5.1.073

• Vibration analysis of functionally graded carbon nanotube-reinforced composite sandwich beams in thermal environment

  Farzad Ebrahimi and Navid Farazmandnia

  Abstract | Full Text (2K)

  pages 107-128.

  DOI: 10.12989/aas.2018.5.1.107

• Using XFEM technique to predict the damage of unidirectional CFRP composite notched under tensile load

  A. Benzaama, M. Mokhtari, H. Benzaama, S. Gouasmi and T. Tamine

  Abstract | Full Text (1K)

  pages 129-139.

  DOI: 10.12989/aas.2018.5.1.129

• Dynamic modeling of nonlocal compositionally graded temperature-dependent beams

  Farzad Ebrahimi and Ramin Ebrahimi Fardshad

  Abstract | Full Text (2K)

  pages 141-164.

  DOI: 10.12989/aas.2018.5.1.141