@article{
 title = {Generalized unsteady embedded Newtonian flow},
 type = {article},
 year = {1975},
 keywords = {Aerodynamic Characteristics,Angle of Attack,Boundary Layer Transition,Dynamic Pressure,Dynamic Support Interference,Flow Characteristics,Hypersonic Flows,Mach Angle,Unsteady Aerodynamics,Wind Tunnel Tests},
 pages = {718-726},
 volume = {12},
 websites = {https://arc.aiaa.org/doi/10.2514/3.27870},
 month = {5},
 day = {23},
 id = {9c00a624-29b2-353c-8ec1-e8f084748615},
 created = {2022-06-15T16:35:08.763Z},
 accessed = {2022-06-15},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-15T16:35:09.425Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {ericcson:jsr:1975},
 private_publication = {false},
 abstract = {An analysis is presented which extends the previously developed unsteady embedded Newtonian theory down to finite supersonic Mach numbers. It is found that Mach number can have a very large influence on the stability characteristics of slender blunted cones, and that there exist cone angle-nose bluntness combinations for which these Mach number effects are minimized. The computed effects of nose bluntness on static and dynamic stability derivatives are in excellent agreement with available experimental data. This also holds true for the highly nonlinear effects of angle of attack. © American Institute of Aeronautics and Astronautics, Inc., 1975, All rights reserved.},
 bibtype = {article},
 author = {Ericsson, Lars E.},
 doi = {10.2514/3.27870},
 journal = {Journal of Spacecraft and Rockets},
 number = {12}
}

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