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TsAGI Science Journal

Publication de 6  numéros par an

ISSN Imprimer: 1948-2590

ISSN En ligne: 1948-2604

IMPROVEMENT OF AERODYNAMICS OF CIVIL PLANE WING HIGH-LIFT DEVICES

Volume 44, Numéro 4, 2013, pp. 447-464
DOI: 10.1615/TsAGISciJ.2013010486
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RÉSUMÉ

The results of experimental investigations of high-lift devices of a civil plane wing are presented. The analysis of flow features has been carried out by both force measurements for different Reynolds numbers and flow visualization using mini-tufts. The proposed improvements have allowed increasing the efficiency of high-lift system and providing a specified level of lift.

CITÉ PAR
  1. Bragin N. N., Ryabov D. I., Skomorokhov S. I., Slitinskaya A. Yu., Study of vortex generator influence on the flow in the wake of high-lift system wing, 1770, 2016. Crossref

  2. Kopiev V. F., Zaytsev M. Yu., Belyaev I. V., Investigation of airframe noise for a large-scale wing model with high-lift devices, Acoustical Physics, 62, 1, 2016. Crossref

  3. Soudakov V. G., Voevodin A. V., Mamonova E. E., Investigations of active and passive flow control on civil aircraft with high-lift configuration, 2027, 2018. Crossref

  4. Bragin N. N., Skomorohov S. I., Slitinskaia A. Yu., Chernyshev I. L., Yanin V. V., On the influence of small-dimensional elements on the aerodynamics of supercritical wings, 2027, 2018. Crossref

  5. Voevodin A. V., Soudakov V. G., Control of Flow Past a Model Aircraft in the Landing Configuration Using Aerodynamic Strakes, Fluid Dynamics, 54, 1, 2019. Crossref

  6. Vorozhbit E. E., Petrov A. V., Soudakov V. G., Experimental Investigation of Local Jets Blowing for Flow Control in the Stream Past the Civil Aircraft Wing, Fluid Dynamics, 57, 6, 2022. Crossref

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