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The Effect of Magnetohydrodynamic (MHD) Energy Bypass on Specific Thrust for a Supersonic Turbojet Engine

by Nasa Technical Reports Server (Ntrs) , Theresa L. Benyo
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Current price ₹1,337.00
Original price ₹1,446.00
Original price ₹1,446.00
Original price ₹1,446.00
(-8%)
₹1,337.00
Current price ₹1,337.00

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Book cover type: Paperback
  • ISBN13: 9781289172879
  • Binding: Paperback
  • Subject: N/A
  • Publisher: Bibliogov
  • Publisher Imprint: Bibliogov
  • Publication Date:
  • Pages: 24
  • Original Price: USD 14.75
  • Language: English
  • Edition: N/A
  • Item Weight: 64 grams
  • BISAC Subject(s): General

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.

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