Low-Order GAM Admire System in Landing Preparation Phase

In this paper the symbolic and numeric computations for the simplified GAM (Generic Aerodynamic Model) Admire system are presented . The numeric computations were performed into the MatLab environment with the aim of pre...

Determining the sensitivity of Data Envelopment Analysis method used in airport benchmarking

In the last decade there were some important changes in the airport industry, caused by the liberalization of the air transportation market. Until recently airports were considered infrastructure elements, and they were...

Subsonic aerodynamics experimental research on gas-dynamic parameters of the flow

Subsonic wind tunnels are generally aerodynamic equipment allowing to obtain in one of their elements, namely in the experimental area where the model is placed, a uniform and stable airflow of determined speed. Wind tu...

Preliminary Design of a LSA Aircraft Using Wind Tunnel Tests

This paper presents preliminary results concerning the design and aerodynamic calculations of a light sport aircraft (LSA). These were performed for a new lightweight, low cost, low fuel consumption and long-range aircra...

“Noui Perspective in Aerodinamica Avionului” - 1925 (selected pages)