The generation of shaft power at hypersonic Mach numbers.

An analysis of the inverted gas turbine cycle applied to aircraft propulsion for the Mach Number range 0 - 6 is summarized and the shaft power potential revealed. [...]

Bibliographic Details
Main Author: Eyre, Frank W.
Other Authors: Mordell, D. (Supervisor)
Format: Others
Language:en
Published: McGill University 1961
Subjects:
Online Access:http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=118158