Hypersonic laminar boundary-layer transition on 8-foot-long, 10 deg cone, M sub 1 equals 9.1-16

Autor:	Henry Nagamatsu, R. E. Sheer, B. C. Graber
Rok vydání:	1967
Předmět:	Stagnation temperature Hypersonic speed Materials science business.industry Turbulent heat transfer Aerospace Engineering Geometry Pitot tube Laminar flow Compressible flow law.invention Boundary layer Optics Cone (topology) law business
Zdroj:	AIAA Journal. 5:1245-1252
ISSN:	1533-385X 0001-1452
DOI:	10.2514/3.4178
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_dedup___::542c755c8296d8de9cb1727295c13d21 https://doi.org/10.2514/3.4178 Zobrazit plný text záznamu