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Fluid Dynamics

, Volume 53, Issue 4, pp 510–516 | Cite as

Static Hysteresis of the Aerodynamic Characteristics of a Model Aircraft in the Landing Regime

  • A. V. Voevodin
  • V. G. Soudakov
Article
  • 5 Downloads

Abstract

Flow past a simplified model of the civil aircraft is numerically investigated in the landing regime. The numerical modeling is performed within the framework of the Reynolds equations. The aerodynamic characteristics of the model are studied. Regimes with the static hysteresis are found.

Keywords

static hysteresis numerical modeling aircraft high-lift wing landing regime 

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  1. 1.Central Aerohydrodynamic Institute (TsAGI)Zhukovsky, Moscow oblastRussia

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