Calculative method for estimating the interference pressure field at zero lift on a symmetrical swept-back wing mounted on a circular cylindrical body

Author: Nielsen, Jack N.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A9E19
Link: https://digital.library.unt.edu/ark:/67531/metadc58327/

< New search