High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane-dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1

Author: Robinson, Harold L.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8H05
Link: https://digital.library.unt.edu/ark:/67531/metadc57949/

< New search