Open AccessTHE CALCULATION AERODYNAMIC CHARACTERISTICS OF A HYBRID AEROSTATIC AIRCRAFT
Author(s) -
Дмитрій Миколайович Зінченко,
Gurkan Ortamevzi,
Ахмад Рахмати
Publication year - 2014
Publication title -
mehanika giroskopičeskih sistem/mehanìka gìroskopìčnih sistem
Language(s) - English
Resource type - Journals
eISSN - 2519-2272
pISSN - 0203-3771
DOI - 10.20535/0203-377127201438208
Subject(s) - aerodynamics , aerospace engineering , computer science , bearing (navigation) , matching (statistics) , engineering , mathematics , artificial intelligence , statistics
The article presents a justification layout a new type aircraft with two different sources lifting force – aerodynamic and aerostatic. Consider especially the exploitation aircraft easier to air, identified key issues research, unresolved tasks, formulated the task. Logged matching aerodynamic profile for bearing surface hybrid aircraft, made its adaptation. Using the method of computational aerodynamics the calculation of the flow around the bearing surface, presents an analysis of the results and conclusions and recommendations are given on an aerodynamic design.