research

Prediction of Helicopter Rotor Hover Performance using High Fidelity CFD Methods

Authors
Publication date
2 June 2017
Publisher
'American Institute of Aeronautics and Astronautics (AIAA)'
Doi

    Abstract

    No abstract available

      Similar works

      Full text

      thumbnail-image

      Available Versions

      Crossref

      redirect
      oaiinfo:doi/10.2514%2F6.2017-3053
      Last time updated on 01/04/2019

      Enlighten

      redirect
      oaioai:eprints.gla.ac.uk:138996
      Last time updated on 18/04/2017