Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel IV : the effect of a constant-chord leading-edge flap at high subsonic speeds

Author: Reed, Verlin D
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A8K19
Link: https://digital.library.unt.edu/ark:/67531/metadc58008/

< New search