Aerodynamic Properties of Wings With Leading-Edge Flaps (Nose Flaps),
Abstract
The work discusses the aerodynamic properties of airfoils with two types of leading edge flaps and with crocodile flaps on the basis of the results of NACA and German wind tunnel investigations published in 1944-1948. Its purpose was to make the information available to designers in the form of an analysis of the pressures on the leading edge of the airfoil. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 15, 1969
- Accession Number
- AD0863957
Entities
People
- Jozef Wysocki
Organizations
- National Air and Space Intelligence Center