@inproceedings{
 title = {Dynamic analysis of atmospheric-entry probes and capsules},
 type = {inproceedings},
 year = {2007},
 pages = {815-832},
 volume = {2},
 websites = {https://arc.aiaa.org/doi/10.2514/6.2007-74},
 publisher = {AIAA Paper 2007-0074},
 id = {fd0480bf-4380-34c6-bf9d-cb98868af178},
 created = {2022-06-15T16:50:47.161Z},
 accessed = {2022-06-15},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-15T16:50:47.867Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {murman:aiaa:2007},
 private_publication = {false},
 abstract = {A Computational Fluid Dynamics analysis of the dynamics of probe and capsule shapes at supersonic flight conditions is performed using an automated, inviscid Cartesian-mesh scheme. This analysis uses static and dynamic free-oscillation simulations to develop static and dynamic aerodynamic coefficients for three configurations: the Viking, Genesis, and Mars Exploration Rover capsules. These computed coefficients are compared against data reduced from ballistic-range free-flight testing. A comparison of data reduction methods for capsule shapes from computational simulations and range data is included. Free-flight simulations agree well with available flight data for both fully-coupled simulations and aerodynamic database fly-throughs based on the developed aerodynamic coefficients. A sensitivity analysis of the aerodynamic coefficients for trajectory simulations at constant altitude is included. Copyright © 2007 by the American Institute of Aeronautics and Astronautics, Inc.},
 bibtype = {inproceedings},
 author = {Murman, Scott M. and Aftosmis, Michael J.},
 doi = {10.2514/6.2007-74},
 booktitle = {45th AIAA Aerospace Sciences Meeting}
}

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