A study of a tab-type or two-piece inlet guide vane for off-design matching of rotor air angles in an axial flow aircraft gas turbine compressor

A study of a tab-type or two-piece inlet guide vane for off-design matching of rotor air angles in an axial flow aircraft gas turbine compressor

Bibliographic Details
Main Author:	Kenyon, Richard Albert, 1933-2021
Format:	Thesis Book
Language:	English
Published:	[Ithaca, N. Y.] 1956
Subjects:	Compressors

Internet

Cornell University

Holdings details from Cornell University
Call Number:	+ Thesis TJ10 1956 K37 Thesis 1956 K37