This paper describes a test system of an 8% scale model of STOL aircraft 'ASKA' with turbine powered simulators tested at the Low Speed Wind Tunnel (6.5m) of National Aerospace Laboratory (NAL). The purpose of the system is to achieve high accurate measurements of aerodynamic forces by eliminating piping interferences. The paper also describes performance of the piping interference elimination function and overall system test results.
Model with Turbine Powered Simulators at NAL's Low Speed Wind Tunnel Facility
2000
70 pages
Report
No indication
English