Numerical Study of Plasma-Assisted Aerodynamic Control for Hypersonic Vehicles. Bisek, N. J., Boyd, I. D., & Poggie, J. Journal of Spacecraft and Rockets, 46(3):568–576, American Institute of Aeronautics and Astronautics Inc., May, 2012. doi abstract bibtex Plasma actuators and various forms of volumetric energy deposition have received a good deal of research attention recently as a means of hypersonic flight control. An open question remains as to whether the required power expenditures for such devices can be achieved for practical systems. To address this issue, a numerical study is carried out for hypersonic flow over a blunt-nose elliptic cone to determine the amount of energy deposition necessary for flight control. Energy deposition is simulated by means of a phenomenological dissipative heating model. A parametric study of the effects of energy deposition is carried outfor several blunt elliptic cone configurations. Three different volumetric energy deposition patterns are considered: a spherical pattern, a "pancake" pattern (oblate spheroid), and a "bean" pattern (prolate spheroid). The effectiveness of volumetric energy deposition for flight control appears to scale strongly with a nondimensional parameter based on the freestream flow kinetic energy flux. Copyright Clearance Center Inc.,.
@article{bisek2012,
title = {Numerical {Study} of {Plasma}-{Assisted} {Aerodynamic} {Control} for {Hypersonic} {Vehicles}},
volume = {46},
doi = {10.2514/1.39032},
abstract = {Plasma actuators and various forms of volumetric energy deposition have received a good deal of research attention recently as a means of hypersonic flight control. An open question remains as to whether the required power expenditures for such devices can be achieved for practical systems. To address this issue, a numerical study is carried out for hypersonic flow over a blunt-nose elliptic cone to determine the amount of energy deposition necessary for flight control. Energy deposition is simulated by means of a phenomenological dissipative heating model. A parametric study of the effects of energy deposition is carried outfor several blunt elliptic cone configurations. Three different volumetric energy deposition patterns are considered: a spherical pattern, a "pancake" pattern (oblate spheroid), and a "bean" pattern (prolate spheroid). The effectiveness of volumetric energy deposition for flight control appears to scale strongly with a nondimensional parameter based on the freestream flow kinetic energy flux. Copyright Clearance Center Inc.,.},
number = {3},
journal = {Journal of Spacecraft and Rockets},
publisher = {American Institute of Aeronautics and Astronautics Inc.},
author = {Bisek, Nicholas J. and Boyd, Iain D. and Poggie, Jonathan},
month = may,
year = {2012},
keywords = {Bow Shock, Flight Control, Freestream Conditions, Hypersonic Flows, Hypersonic Vehicles, Pressure Coefficient, Thermal Nonequilibrium, Thermal Protection System, Vibrational Energy, Wall Temperature},
pages = {568--576},
}
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