NASA NTRS · 19930081042
The NACA CYH Airfoil Section
Abstract
The NACA CYH airfoil section is described and its aerodynamic characteristics are given as tested in the NACA variable density wind tunnel at twenty atmosphere pressure. This section has a low drag, a high maximum lift, and a small travel of center of pressure.
Keep this discovery
Explore connections, maps & timelines
Higgins, George J. 1926-06-01. The NACA CYH Airfoil Section. https://ntrs.nasa.gov/citations/19930081042
Cite the original work for its findings. Save a collection to share your selection of sources.