Validation and Benefits of a Homogeneous Effusion Cooling Model for Combustor RANS Simulations
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 16289-16301
2009-01-01
13 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Numerical Benchmark of Nonconventional RANS Turbulence Models for Film and Effusion Cooling
Online Contents | 2013
|Exploratory RANS and LES Simulations of Transient Supersonic Combustor Flow
British Library Conference Proceedings | 2009
|