Investigation at high and low subsonic Mach numbers of two symmetrical 6-percent-thick airfoil sections designed to have high maximum lift coefficients at low speeds

Author: Paradiso, Nicholas J.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52I02
Link: https://digital.library.unt.edu/ark:/67531/metadc59367/

< New search