Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01

Author: Lord, Douglas R.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L58C07
Link: https://digital.library.unt.edu/ark:/67531/metadc64060/

< New search