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

Volume

1

fYear

1999

fDate

1999

Firstpage

58

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;

fLanguage

English

Publisher

ieee

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

Type

conf

DOI

10.1109/KORUS.1999.875867

Filename

875867