FIELD: aircraft engineering. SUBSTANCE: air intake is mounted under aerodynamic surface 1 of the flying vehicle and has vertical compression wedges 2 and 3, shell 4. Leading edges of the compression wedges are made with negative sweep angle χ relative to the normal to the aerodynamic surface. EFFECT: improved structure. 1 dwg
Authors
Dates
1994-08-15—Published
1991-11-12—Filed