Measurements of Aerodynamic Characteristics of a 35 deg Sweptback NACA 65-009 Airfoil Model with 1/4-Chord Plain Flap by the NACA Wing-Flow Method
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 05, 1947
- Accession Number
- ADA800754
Entities
Organizations
- Langley Research Center