Development of the Aircraft In-Flight Loads Computer Software

Principal Investigator’s Organization (PIO):

CASE, Islamabad

Principal Investigator (PI):

Dr. Saeed Ur Rehman
Dr. Haroon Awais Baluch


In this project a software was developed, for solving fully integrated aeroservoelastic (ASE) system, apart from the structural loads. It contains the unsteady aerodynamics solver to compute the air loads on the aircraft, the structural dynamics solver to compute the vibration characteristics of the aircraft structure and lastly the flight dynamics with controls solver to compute the rigid-body dynamics of the aircraft.