Computer Aided Performance Analysis of Jet and Propeller Aircraft

Computer Aided Performance Analysis of Jet and Propeller Aircraft
Author: Stuart Bennett Schapiro
Publisher:
Total Pages: 466
Release: 1988
Genre:
ISBN:

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Computer Aided Performance Analysis of Jet and Propeller Aircraft
Language: en
Pages: 466
Authors: Stuart Bennett Schapiro
Categories:
Type: BOOK - Published: 1988 - Publisher:

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Computer and Engine Performance Study of a Generalized Parameter Fuel Control for Jet Engines
Language: en
Pages: 42
Authors: Kurt Seldner
Categories: Airplanes
Type: BOOK - Published: 1970 - Publisher:

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A mathematical analysis of a generalized parameter hydraulic fuel control concept is presented. An analog computer simulation was used to establish the feasibil
Commercial Aircraft Propulsion and Energy Systems Research
Language: en
Pages: 123
Authors: National Academies of Sciences, Engineering, and Medicine
Categories: Technology & Engineering
Type: BOOK - Published: 2016-08-09 - Publisher: National Academies Press

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The primary human activities that release carbon dioxide (CO2) into the atmosphere are the combustion of fossil fuels (coal, natural gas, and oil) to generate e
Performance Analysis of J85 Turbojet Engine Matching Thrust with Reduced Inlet Pressure to the Compressor
Language: en
Pages: 87
Authors: Santosh Yarlagadda
Categories: Airplanes
Type: BOOK - Published: 2010 - Publisher:

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Jet engines are required to operate at a higher rpm for the same thrust values in cases such as aircraft landing and military loitering. High rpm reflects highe
An Introduction to Thermodynamic Performance Analysis of Aircraft Gas Turbine Engine Cycles Using the Numerical Propulsion System Simulation Code
Language: en
Pages: 46
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-05-20 - Publisher: Createspace Independent Publishing Platform

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This document is intended as an introduction to the analysis of gas turbine engine cycles using the Numerical Propulsion System Simulation (NPSS) code. It is as