Pressure distribution on helicopter fuselage by Aris, Anas Faiz, Ishak, Iskandar Shah, Ali, Airi, Othman, Norazila

“…Results also indicate the pressure distributions on the right and left sides of the fuselage are unsymmetrical indicating a very complex flow phenomenon experienced by the helicopter fuselage.…”
Get full text

Static analysis of unsteady aerodynamics wake of simplified helicopter model via simulation work by Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam

“…The study also examined the unsteady flow behaviour on the three-dimensional elliptical shape of a fuselage equipped with a rotor hub of the single rotor blade. …”
Get full text

Unsteady aerodynamic wake of helicopter main-rotor-hub assembly by Ishak, Iskandar Shah

“…In this research work, a simplified NASA standard fuselage model was mated to a main-rotor-hub assembly from a remote-control helicopter. …”
Get full text

Comparison on the aerodynamic coefficients obtained from three different size of wind tunnel model on Baseline V set at 45 degree sweep tail angle by Abd. Latif, Mohamad Zulfazli Arief, Mohd. Nasir, Rizal Effendy, Ahmad, Muhammad Aiman, Wisnoe, Wirachman, Kuntjoro, Wahyu, Ishak, Iskandar Shah, Saad, M. R. S.

“…Base-line V is one of the Universiti Teknologi MARA (UiTM) Shah Alam Flight Test Technology Centre's blended wing body designs that have unique configuration as it uses different NACA airfoil for its fuselage, body, wing root, midwing, wingtip, tail root, and tail tip. …”
Get full text