Simulations of an aircraft with constant and pulsed blowing flow control at the engine/wing junction-Reference-Cited by-同舟云学术

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Simulations of an aircraft with constant and pulsed blowing flow control at the engine/wing junction

Published:2017-10 Issue: Volume:69 Page:659-673
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hue David,François Christophe,Dandois Julien,Gebhardt Anna

Funder

Seventh Framework Programme

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. Stall Behaviour of the EUROLIFT High Lift Configurations;Rudnik,2008

2. CFD Prediction of Maximum Lift Effects on Realistic High-Lift-Commercial-Aircraft-Configurations Within the European Project EUROLIFT II;Geyr,2007

3. Active flow control applied at the engine-wing junction;Fricke,2015

4. Numerical studies of active flow control applied at the engine-wing junction;Fricke,2016

5. Overview of ONERA actuators for active flow control;Ternoy;AerospaceLab,2013

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4. Experimental Investigation of Local Jets Blowing for Flow Control in the Stream Past the Civil Aircraft Wing;Fluid Dynamics;2022-11-29

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