A theoretical analysis of the performance of a diesel engine-compressor-turbine combination for aircraft Page: 1 of 25
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
ACR No. E5DO1
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
WA II IE REPO T
April 1945 as
Advance Confidential Report E5D10
A THEORETICAL ANALYSIS OF THE PERFORMANCE OF A DIESEL
ENGINE -COMPRESSOR-TURBINE COMBINATION FOR AIRCRAFT
By Eldon W. Hall
Aircraft Engine Research Laboratory
N A C A LIB'V m
WASHINGTON LAC MEMORIAL A .
LABORN, Tr;, ,r
NACA WARTIME REPORTS are reprints of papers originally issued to provide api d o nibutoin of
advance research results to an authorized group requiring them for the war effo RreWe'Ae re-
viously held under a security status but are now unclassified. Some of these reports were not tech-
nically edited. All have been reproduced without change in order to expedite general distribution.
DEC 93 1946
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Hall, Eldon W. A theoretical analysis of the performance of a diesel engine-compressor-turbine combination for aircraft, report, April 1, 1945; (digital.library.unt.edu/ark:/67531/metadc62106/m1/1/: accessed December 17, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.