An integral solution to the flat-plate laminar boundary-layer flow existing inside and after expansion waves and after shock waves moving into quiescent fluid with particular application to the complete shock-tube flow

Author: Trimpi, Robert L
Year: 1957
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3944
Link: https://digital.library.unt.edu/ark:/67531/metadc56219/

< New search