@article{
 title = {Unsteady embedded Newton-Busemann flow theory},
 type = {article},
 year = {1986},
 keywords = {Angle of Attack,Conservation of Mass,Flight Path Angle,Freestream Mach Number,Hypersonic Flight,Hypersonic Flows,Mass Flow Rate,Shock Layers,Specific Heat,Taylor Series},
 pages = {129-135},
 volume = {23},
 websites = {https://arc.aiaa.org/doi/10.2514/3.25798},
 month = {5},
 day = {23},
 id = {3567b87b-43ba-3edd-8e85-d67434ccf4fa},
 created = {2022-06-15T16:33:26.881Z},
 accessed = {2022-06-15},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-15T16:33:27.584Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {tong:jsr:86},
 private_publication = {false},
 abstract = {An unsteady, embedded Newton-Busemann flow theory is developed by extending the unsteady Newton- Busemann flow theory of Hui and Tobak to blunt bodies, incorporating the embedded Newtonian flow concept of Seiff and Ericsson. In this theory the unsteady surface pressure includes the Newtonian impact part plus Busemann’s centrifugal correction. Applications to dynamic stability of blunt bodies of revolution show that 1) the centrifugal pressure is just as important as the impact part and must not be neglected and 2) with its inclusion the complete theory is in good agreement with existing experiments for high Mach number flow. © American Institute of Aeronautics and Astronautics, Inc., 1986, All rights reserved.},
 bibtype = {article},
 author = {Tong, Bing Gang and Hui, W. H.},
 doi = {10.2514/3.25798},
 journal = {Journal of Spacecraft and Rockets},
 number = {2}
}

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