@article{
 title = {Numerical Study of Plasma-Assisted Aerodynamic Control for Hypersonic Vehicles},
 type = {article},
 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},
 volume = {46},
 month = {5},
 publisher = {American Institute of Aeronautics and Astronautics Inc.},
 day = {23},
 id = {de9d4be7-3f62-3a10-b9fb-633cb9917241},
 created = {2022-06-08T19:32:01.064Z},
 accessed = {2022-06-08},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-08T19:32:02.071Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {bisek:jsr:2012},
 private_publication = {false},
 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.,.},
 bibtype = {article},
 author = {Bisek, Nicholas J. and Boyd, Iain D. and Poggie, Jonathan},
 doi = {10.2514/1.39032},
 journal = {Journal of Spacecraft and Rockets},
 number = {3}
}

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