Title: Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
First published: 1994
Subjects: Aerodynamic characteristics, Angle of attack, Buffeting, Flight tests, Flow visualization, Liquid-vapor interfaces, Scale models, Sideslip, Stabilizers (Fluid dynamics), Tail assemblies, Vortices, Water tunnel tests, X-29 aircraft