METHOD FOR NUMERICAL MODELING OF UNSTEADY SEPARATED FLOW AROUND AIRFOILS MOVING CLOSE TO FLAT SCREEN

In this article an attempt is made to explain the nature of differences in measurements of forces and moments, which influence an aircraft at take-off and landing when testing on different types of stands. An algorithm for numerical simulation of unsteady separated flow around airfoil is given. The...

Täydet tiedot

Tallennettuna:
Bibliografiset tiedot
Päätekijät: T. V. Pogrebnaya, S. D. Shipilov
Aineistotyyppi: Artigo
Kieli:Russo
Julkaistu: Moscow State Technical University of Civil Aviation 2017-05-01
Sarja:Naučnyj Vestnik MGTU GA
Aiheet:
unsteady aerodynamics
airfoil
screen
method of discrete vortices
boundary layer
mirror method
fixed or movable screens
Linkit:https://avia.mstuca.ru/jour/article/view/1056
Tagit: Lisää tagi
Ei tageja, Lisää ensimmäinen tagi!

Samankaltaisia teoksia