Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Investigation of the Stabilator on the S-67 Aircraft
Helicopter Vertical Stabilizer Design Considerations
Transonic Flutter Characteristics of a 45 Degree Swept Back All Movable Stabilizer
Stability of Structure Following Bird Strike
Flutter Clearance of the Horizontal Tail of the Bellanca Skyrocket II Airplane
Cost Effectiveness of Composite Materials on the F-15 and F-16 Aircrafts
Research and Development of Control Actuation Systems for Aircraft. Volume I
Procedures and Design Data for the Formulation of Aircraft Configurations
Development of Stall Deterrent Concepts for General Aviation Aircraft
Report on Proceedings Held by the Wglr Committee on Aerodynamics, on July 10, 1967 in Darmstadt
Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft
Autorotational Entry Improvement Program TH-55A Helicopter
Feasibility Study of the CH-53A Horizontal Stabilizer as an HF Antenna