Accession Number:

ADB805892

Title:

A Theoretical Analysis of the Performance of a Diesel Engine Compressor Turbine Combination for Aircraft

Descriptive Note:

Wartime rept.

Corporate Author:

AIRCRAFT ENGINE RESEARCH LAB CLEVELAND OH

Personal Author(s):

Report Date:

1945-04-01

Pagination or Media Count:

34.0

Abstract:

Subject Categories:

  • Reciprocating and Rotating Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE