HIGH LIFT SURFACE DESIGN PROCEDURES. EXPERIMENTAL VERIFICATION. VOLUME II. THEORETICAL DESIGN AND ANALYSIS.
Abstract
The development of four wings which were designed to have specific aerodynamic requirements is described. The wings designed were: a high lift wing, a low lift or cruise wing, both of which were smooth, and two flapped wings which were approximations of the smooth wings.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1966
- Accession Number
- AD0639289
Entities
People
- J. R. Stevens
- J. W. Headley
- J. W. Mcdonald