Noise Estimation of Beveled Trailing Edges Using an Integral and Boundary Element Method (AIAA 2016-0260)
Aerospace sciences meeting
01.01.2016
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
2D Steady Wake Predictions for Airfoil Cascades with Beveled Trailing Edges
British Library Conference Proceedings | 1997
|Wake Development of Airfoils with Serrated Trailing Edges (AIAA 2016-2817)
British Library Conference Proceedings | 2016
|British Library Conference Proceedings | 2015
|