Vol 23 No 4 (2019)

Published: 2020-02-17

Articles

  • Wind tunnel calibration, corrections and experimental validation for fixed-wing micro air vehicles measurements

  • Numerical analysis of the impact of sideslip angle on load of the gyrocopter stabilizers

  • Towards meeting the IATA-agreed 1.5% average annual fuel efficiency improvements between 2010 and 2020: the current progress being made by U.S. air carriers

  • Developed criteria to improve pilot reporting of airplane vortex encounters

  • Model predictive control of a hydraulic actuator in torque applying system of a mechanically closed-loop test rig for the helicopter gearbox