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Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer

Aerospace Corporation

出版	1963
URL	http://books.google.com.hk/books?id=l-BYAAAAYAAJ&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent wall boundary layers. The results are compared with those for wholly laminar wall boundary layers. Working curves are presented for more accurate estimates of test time in specific cases. (Author) -- NTRL website.