المؤلفون: Puopolo, Michael G., Reynolds, Ryan, Jacob, Jamey D.

المصدر: Mechanical and Aerospace Engineering Faculty Research & Creative Works

مصطلحات موضوعية: Aerodynamic modeling, Aerodynamic models, Flat-plate theory, High angle of attack, Lift and drag coefficients, Oklahoma State University, Output parameters, Simulated flight, Aerospace engineering, Angle of attack, Computer simulation, Mechanical Engineering

العلاقة: https://scholarsmine.mst.edu/mec_aereng_facwork/4302Test; https://doi.org/10.2514/6.2013-242Test

الإتاحة: https://doi.org/10.2514/6.2013-242Test
https://scholarsmine.mst.edu/mec_aereng_facwork/4302Test

المؤلفون: Atilla Dogan, Yasmina Bestaoui, Jayme Waishek

المساهمون: Department of Mechanical and Aerospace Engineering, University of Texas at Arlington [Arlington], Informatique, Biologie Intégrative et Systèmes Complexes (IBISC), Université d'Évry-Val-d'Essonne (UEVE), Davesne, Frédéric

المصدر: Proc. of the AIAA Atmospheric Flight Mechanics Conference 2010
AIAA Atmospheric Flight Mechanics Conference 2010
AIAA Atmospheric Flight Mechanics Conference 2010, Aug 2010, Toronto, ON, Canada. (elec. proc)
Scopus-Elsevier

مصطلحات موضوعية: Engineering, Flight test, business.industry, Control mechanism, Inertia properties, Aerodynamic models, Prevailing winds, Aerospace engineering, business, Physics::Atmospheric and Oceanic Physics, Time-varying inertia, Characterization (materials science), Time varying

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7c9d594d70e7969031d595fb14fb3e8aTest
https://hal.archives-ouvertes.fr/hal-00869232Test