Studies and Research on Applied Mechanics (Selected Articles).
Abstract
Contents: The Supersonic Flow Around Symmetrical Torsioned and Curved Delta Wings, Taking Into Consideration the Separation of Flow at the Leading Edges; and The Thin Delta Wing, With Variable Geometry, Optimum for Two Supersonic Cruising Speeds.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 30, 1978
- Accession Number
- ADA061935
Entities
Organizations
- National Air and Space Intelligence Center