Preliminary Results of an Altitude-Wind-Tunnel Investigation of an Axial-Flow Gas Turbine-Propeller Engine: Compressor and Turbine Performance Characteristics - 4
20030065929 · NASA · 1948
Public domain · NASATechnical Reports
Overview
As part of an investigation of the performance and operational characteristics of the axial-flow gas turbine-propeller engine, conducted in the Cleveland altitude wind tunnel, the performance characteristics of the compressor and the turbine were obtained. The data presented were obtained at a…
- Publisher
- NASA
- Document
- 20030065929
- Year
- 1948
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
Permanent URL — we don’t break links.
Document details
- Doc number
- 20030065929
- Publisher
- NASA
- Year
- 1948
- File size
- 1.0 MB