Zobrazeno 1 - 7
of 7
pro vyhledávání: '"B. C. Graber"'
Publikováno v:
Proceeding of International Heat Transfer Conference 3.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f16a88766662ab071dae8cc81937aeb
https://doi.org/10.1615/ihtc3.1800
https://doi.org/10.1615/ihtc3.1800
Publikováno v:
AIAA Journal. 5:1245-1252
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::542c755c8296d8de9cb1727295c13d21
https://doi.org/10.2514/3.4178
https://doi.org/10.2514/3.4178
Publikováno v:
Journal of Fluid Mechanics. 24:1-31
An investigation was conducted in a hypersonic shock tunnel to study the laminar boundary-layer transition on a highly cooled 10° cone of 4 ft. length over the Mach-number range of 8·5 to 10·5 with a stagnation temperature of 1400 °K. The effects
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::521d5059bf725aba91afb2720f38b164
https://doi.org/10.1017/s002211206600048x
https://doi.org/10.1017/s002211206600048x
Publikováno v:
AIAA Journal. 1:2173-2175
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::355a03188da7afea93c4deb2df9ebbc4
https://doi.org/10.2514/3.2028
https://doi.org/10.2514/3.2028
Publikováno v:
Aircraft Design and Technology Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de2b6d89af2bfce8d4f793b7a7f6cdc4
https://doi.org/10.2514/6.1965-754
https://doi.org/10.2514/6.1965-754
Publikováno v:
Physics of Fluids. 8:211
An investigation was conducted in a hypersonic shock tunnel to study the boundary layer on a 10° cone of 4 ft length having a wall to stagnation temperature ratio of 0.214. An impact pressure survey of the various types of boundary layer flows was m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00785eb73bc0f6b0be3ee6a8eeed5082
https://doi.org/10.1063/1.1761211
https://doi.org/10.1063/1.1761211