AN INVESTIGATION AT TRANSONIC SPEEDS OF THE EFFECTS OF FENCES, DROOPED NOSE, AND VORTEX GENERATORS ON THE AERODYNAMIC CHARACTERISTICS OF A WING-FUSELAGE COMBINATION HAVING A 6-PERCENT-THICK, 45 DEG SWEPTBACK WING
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 31, 1953
- Accession Number
- AD0005949
Entities
People
- Gerald Hieser
Organizations
- Langley Research Center