NACA-RM-E8H06 · Preliminary Results of Nene II Engine Altitude-chamber Performance Investigation: Altitude Performance using 18.00-inch-diameter Jet Nozzle - 3
NASA (NTRS) · 1948
Overview
An investigation is being conducted to determine the altitude performance characteristics of the Nene II engine and its components. The present paper presents the preliminary results obtained using jet nozzle 18.00 inches in diameter, with an area equal to 92.2 percent of the area of the standard…
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 ·
- NACA-RM-E8H06
- Publisher ·
- NASA (NTRS)
- Year ·
- 1948
- File size ·
- 7.6 MB