Actions for Theoretical investigation of velocity diagrams of a single-stage turbine for a turbojet engine at maximum thrust per square foot turbine frontal area

Email RIS file
Bookmark
Report an Issue

Theoretical investigation of velocity diagrams of a single-stage turbine for a turbojet engine at maximum thrust per square foot turbine frontal area

Author
Cohen, Leo
Physical Description
1 electronic document
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930083384.
Accession ID: 93R12674.
NACA-TN-2732.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15434119