A nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison

Author:	Trimpi, Robert L
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4347
Link:	https://digital.library.unt.edu/ark:/67531/metadc57216/