This book includes a collection of chosen research papers from the partners of a research project (the Seventh Framework Programme Grant Agreement (Grant Number: 266326)) named Manipulation of Reynolds Stress for Separation Control and Drag Reduction (MARS) conducted between 2010 and 2014. The project is jointly funded by the European Commission (EC) and the Ministry of Industrial and Information Technology (MIIT) of China. As you will notice, many of the papers reflect the bilateral EU-China collaborations as a result of the project. The MARS consortium was led by International Centre for Numerical Methods in Engineering (CIMNE) in Spain and the University of Sheffield in UK on the European side, Chinese Aeronautical Establishment (CAE) an...
Additional results about the wing-body of the NASA Common Research Model at flight conditions derive...
The Energy System Transition in Aviation research project of the Aeronautics Research Center Nieder...
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as prese...
A hot topic in today's debate on global warming is drag reduction in aeronautics. The most beneficia...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
A hot topic in today's debate on global warming is drag reduction in aeronautics. The most benecial ...
This book explores the outcomes on flow control research activities carried out within the framework...
The reduction of drag on commercial aircraft is an active field of study especially with environment...
A combined computational and experimental effort has been undertaken to study fuselage drag reductio...
The Computational Flow Control (CFC) Research Group is investigating mechanisms and applications of ...
The European Drag Reduction Meeting has been held on 15th and 16th November 1990 in London. This was...
The reduction of drag on commercial aircraft is an active field of study especially with environment...
The final publication is available at Springer via http://dx.doi.org/10.1007/s11431-016-9013-6Turbul...
This article is placed here with permission from the Royal Aeronautical Society - Copyright @ 2009 R...
This book explores the outcomes on flow control research activities carried out within the framework...
Additional results about the wing-body of the NASA Common Research Model at flight conditions derive...
The Energy System Transition in Aviation research project of the Aeronautics Research Center Nieder...
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as prese...
A hot topic in today's debate on global warming is drag reduction in aeronautics. The most beneficia...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
A hot topic in today's debate on global warming is drag reduction in aeronautics. The most benecial ...
This book explores the outcomes on flow control research activities carried out within the framework...
The reduction of drag on commercial aircraft is an active field of study especially with environment...
A combined computational and experimental effort has been undertaken to study fuselage drag reductio...
The Computational Flow Control (CFC) Research Group is investigating mechanisms and applications of ...
The European Drag Reduction Meeting has been held on 15th and 16th November 1990 in London. This was...
The reduction of drag on commercial aircraft is an active field of study especially with environment...
The final publication is available at Springer via http://dx.doi.org/10.1007/s11431-016-9013-6Turbul...
This article is placed here with permission from the Royal Aeronautical Society - Copyright @ 2009 R...
This book explores the outcomes on flow control research activities carried out within the framework...
Additional results about the wing-body of the NASA Common Research Model at flight conditions derive...
The Energy System Transition in Aviation research project of the Aeronautics Research Center Nieder...
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as prese...