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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: T. V. Pogrebnaya, S. D. Shipilov
Format: Artigo
Sprache:Russo
Veröffentlicht: Moscow State Technical University of Civil Aviation 2017-05-01
Schriftenreihe:Naučnyj Vestnik MGTU GA
Schlagworte:
unsteady aerodynamics
airfoil
screen
method of discrete vortices
boundary layer
mirror method
fixed or movable screens
Online Zugang:https://avia.mstuca.ru/jour/article/view/1056
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