Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having aspect ratios of 1.5 and 2.7 as determined by flight tests at supersonic speeds

Author: Alexander, Sidney R.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L6J16
Link: https://digital.library.unt.edu/ark:/67531/metadc58091/

< New search