Effects of film injection angle on turbine vane cooling

Contributor(s): Language: English Series: NASA TP 1095 : 1977Publication details: Washington, D.C. ; National Aeronautics and Space Administration ; 1977Edition: Description: 23 p; ISBN: Subject(s): | Heat transfer, Film cooling, Turbine bladesOnline resources: Click here to access online
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA TP 1095 : 1977 Not for loan A37842
Total holds: 0

There are no comments on this title.

to post a comment.
Share

Powered by Koha