UNT Digital Library
metadata only
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 3 - 18.00-Inch-Diameter Jet Nozzle
An altitude-chamber investigation of British Rolls-Royce Nene II turbojet engine was conducted over range of altitudes from sea level to 65,000 feet and ram pressure ratios from 1.10 to 3.50, using an 18.00-inch-diameter jet nozzle. The 18.00-inch-diameter jet nozzle gave slightly lower values of ne
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- An investigation into the pitot rake method of measuring turbo jet engine thrust in flight#491495
- Acord - cadru furnizare combustibil pentru turboreactoare de aviație tip JET A1 pe aeroportul Satu Mare#382195
- Acord - cadru furnizare combustibil pentru turboreactoare de aviație tip JET A1 pe aeroportul Suceava#382198
- Acord - cadru furnizare combustibil pentru turboreactoare de aviație tip JET A1 pe aeroportul Sibiu#382199
- Generalization of Neutrosophic Rings and Neutrosophic Fields#93097
Record · ID 1278404
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive