The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine /

Bibliographic Details

Main Author:	Benyo, Theresa L.
Corporate Authors:	NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216734.
Subjects:	Magnetohydrodynamics. Thermodynamic cycles. Turbojet engines. Thermal conductivity. Supersonic speed. Specific impulse. Enthalpy. Hypersonic flight.
Online Access:	https://purl.fdlp.gov/GPO/gpo8575