Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections

Author: Wilson, Homer B., Jr.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52G17
Link: https://digital.library.unt.edu/ark:/67531/metadc59310/

< New search