Title :
The calculation of the three-dimensional boundary layer at the turn of the flow on the circular sector
Author :
Kraev, M.V. ; Kishkin, A.A. ; Chernenko, D.V. ; Melkozerov, M.G.
Author_Institution :
Siberian Aerosp. Acad., Krasnoyarsk, Russia
Abstract :
The considerable range of problems, connected with the motion of the flow in the flowing part of flying machine engines, is connected with the possibility of the boundary layer equation integration along the complex surface with transverse pressure gradient. For the choice of the solution method and for the construction of the calculation algorithm the three-dimensional boundary layer (TDBL) momentum´s equations system need to result in a form which is defined on variables and permits one to conduct both the numerical integration in the common case and analytical analysis in individual cases
Keywords :
aerospace engines; boundary layers; integration; boundary layer equation integration; circular sector; flow motion; flying machine engines; numerical integration; three-dimensional boundary layer; transverse pressure gradient; Aerospace industry; Algorithm design and analysis; Differential equations; Engines; Friction;
Conference_Titel :
Science and Technology, 1999. KORUS '99. Proceedings. The Third Russian-Korean International Symposium on
Conference_Location :
Novosibirsk
Print_ISBN :
0-7803-5729-9
DOI :
10.1109/KORUS.1999.875867
