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Comparisons of Turbulent-boundary-layer Measurements at Mach Number 19.5 with Theory and an Assessment of Probe Errors
Ivan E. Beckwith
Frank L. Clark
William D. Harvey
出版
National Aeronautics and Space Administration
, 1971
URL
http://books.google.com.hk/books?id=WBUHQSJAMvYC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
Measurements of total temperature and pitot pressure across boundary layer of test section wall of axisymmetric contoured nozzle at hypersonic speed in nitrogen.
