Thomas N. Aiken

Full-scale Wind-tunnel Tests of a Small Unpowered Jet Aircraft with a T-Tail

The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 me...

Stability and Control Characteristics of a Large-scale Deflected Slipsteam STOL Model with a Wing of 5.7 Aspect Ratio

Wind tunnel tests of stability and control characteristics of large scale model representative of propeller-driven STOL transport aircraft....