The Effect Of Magnetohydrodynamic (mhd) Energy Bypass On Specific Thrust For A Supersonic Turbojet Engine

by Nasa Technical Reports Server (ntrs)

2021-01-13 21:10:19

This paper describes the preliminary results of a thermodynamic cycle analysis of a supersonic turbojet engine with a magnetohydrodynamic (MHD) energy bypass system that explores a wide range of MHD enthalpy extraction parameters. Through the analysi... Read more
This paper describes the preliminary results of a thermodynamic cycle analysis of a supersonic turbojet engine with a magnetohydrodynamic (MHD) energy bypass system that explores a wide range of MHD enthalpy extraction parameters. Through the analysis described here, it is shown that applying a magnetic field to a flow path in the Mach 2.0 to 3.5 range can increase the specific thrust of the turbojet engine up to as much as 420 N/(kg/s) provided that the magnitude of the magnetic field is in the range of 1 to 5 Tesla. The MHD energy bypass can also increase the operating Mach number range for a supersonic turbojet engine into the hypersonic flight regime. In this case, the Mach number range is shown to be extended to Mach 7.0. Less

Book Details

File size9.69 X 7.44 X 0.05 in
Print pages24
PublisherBiblioGov
Publication date July 16, 2013
LanguageEnglish
ISBN9781289172879

Compare Prices

Store Availability Book Format Condition Price
Indigo Books & Music In Stock Paperback Paperback Buy CAD 16.99
Indigo Books & MusicIn Stock
Format
Paperback
Condition
Paperback
Buy CAD 16.99
Available Discount
No Discount available

Join us and get access to all
your favourite books

Sign up for free and start exploring thousands of eBooks today.

Sign up for free