20030063965 · Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine: Compressor and Turbine Performance Characteristics - 4
NASA · 1947
Overview
As part of an investigation of the performance and operational characteristics of the TG-100A 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…
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
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Document details
- Doc number ·
- 20030063965
- Publisher ·
- NASA
- Year ·
- 1947
- File size ·
- 1.1 MB