Gas turbine engine thrust
id:
gas-turbine-engine-thrust-179-4240218
title:
Gas turbine engine thrust
text:
The familiar study of jet aircraft treats jet thrust with a "black box" description which only looks at what goes into the jet engine, air and fuel, and what comes out, exhaust gas and an unbalanced force. This force, called thrust, is the sum of the momentum difference between entry and exit and any unbalanced pressure force between entry and exit, as explained in "Thrust calculation". As an example, an early turbojet, the Bristol Olympus Mk. 101, had a momentum thrust of 9300 lb. and a pressur
brand slug:
wiki
category slug:
encyclopedia
description:
original url:
https://en.wikipedia.org/wiki/Gas_turbine_engine_thrust
date created:
2018-10-23T14:45:37Z
date modified:
2024-09-04T23:18:32Z
main entity:
{"identifier":"Q60749961","url":"https://www.wikidata.org/entity/Q60749961"}
image:
fields total:
13
integrity:
14