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Title: MHD of Aircraft Re-entry: Limits and Perspectives

Journal Article · · AIP Conference Proceedings
DOI:https://doi.org/10.1063/1.1941707· OSTI ID:20722267
 [1]; ;  [2]; ;  [3]
  1. Dipartimento di Scienze e Tecnologie Fisiche ed Energetiche, Tor Vergata University, Via di Tor Vergata 110, 00133 Rome (Italy)
  2. Chemistry Department, Bari University, Via Orabona 4, 70126 Bari (Italy)
  3. IMIP-CNR, Via Orabona 4, 70126 Bari (Italy)

In the present work, starting from classical MHD scheme, based on Maxwell equations, Euler fluid dynamic equations and generalised Ohm law, a critical study of fluid dynamics, electromagnetism, chemical and physical behaviour of plasma is carried out, and then a aircraft re-entry MHD numerical scheme is implemented. This scheme is used for MHD calculations in different conditions, in the range of low magnetic force and intermediate electrical conductivity. Initial imposed magnetic fields are uniform, but also some cases with coil generated magnetic fields are considered. Calculations of magnetic field and induced currents are extended also inside the blunt body. Results show interesting physical and electromagnetic effects. Comparison with other methods shows possible development in keeping into account other physical and chemical effects.

OSTI ID:
20722267
Journal Information:
AIP Conference Proceedings, Vol. 762, Issue 1; Conference: 24. international symposium on rarefied gas dynamics, Bari (Italy), 10-16 Jul 2004; Other Information: DOI: 10.1063/1.1941707; (c) 2005 American Institute of Physics; Country of input: International Atomic Energy Agency (IAEA); ISSN 0094-243X
Country of Publication:
United States
Language:
English