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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/
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