Possibility of thermal protection in earth re-entry flight by MHD flow control with air-core circular magnet

IEEJ Transactions on Electrical and Electronic Engineering

Volumn 4, Issue 4, 2009, Pages 510-517

  Yoshino, Tomoyuki ^a   Fujino, Takayasu ^a   Ishikawa, Motoo ^a  

^a UNIVERSITY OF TSUKUBA   (Japan)

Author keywords

Convection heat transfer; Flow control with electromagnetic force; Weakly ionized plasma flow

Indexed keywords

AERODYNAMICS; EARTH (PLANET); FLIGHT SIMULATORS; FLOW CONTROL; HEAT CONVECTION; HEAT EXCHANGERS; MAGNETS; NUMERICAL ANALYSIS; PLASMA DEVICES; PLASMA FLOW; PLASMA JETS; REENTRY; TWO DIMENSIONAL; VEHICLES;

AIR-CORE; COIL CURRENT; CONVECTION HEAT TRANSFER; ELECTROMAGNETIC FORCES; FLIGHT ALTITUDES; MAGNETIC ENERGIES; MAGNETOHYDRODYNAMIC FLOWS; MHD FLOW; NUMERICAL RESULTS; SPACE VEHICLES; THERMAL PROTECTION; TWO-DIMENSIONAL NUMERICAL SIMULATION; WALL HEAT FLUX; WALL SURFACES; WEAKLY IONIZED PLASMA;

ALTITUDE CONTROL;

EID: 77749315421     PISSN: 19314973     EISSN: 19314981     Source Type: Journal    
DOI: 10.1002/tee.20437     Document Type: Article

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