๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Transition modelling for the prediction of the heat transfer coefficient of a gas-turbine blade

โœ Scribed by B.A. Jubran; M.A. Hamdan; A.I. Al-Sayeh


Publisher
Elsevier Science
Year
1994
Tongue
English
Weight
565 KB
Volume
49
Category
Article
ISSN
0306-2619

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


The interior heat transfer characteristi
โœ Zhang Jingyu; Chang Haiping ๐Ÿ“‚ Article ๐Ÿ“… 2005 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 213 KB

The film cooling technique is one of the most useful cooling methods. At present, the midchord region of gas turbine blades in an aeroengine often adopt a sparse film cooling technique and impingement cooling technique at the same time. So the interior heat transfer characteristics on the inner side

Some models for the calculation of heat
โœ J.W. Rotte; W.J. Beek ๐Ÿ“‚ Article ๐Ÿ“… 1969 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 778 KB

When a contmuous cylmder IS cooled by passmg lt longltudmally through a qmet flmd (free convecfion IS not consldered) then the followmg relatlon for the local heat transfer coefficlent can be glven The group d(Pรฉ,)/P&. allows for the curvature of the cylmder. the fourth dlmenslonless group accommoda