Model for investigation of helicopter fuselage influence on rotor flowfields
- 1 May 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (5) , 401-402
- https://doi.org/10.2514/3.45775
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Calculation of potential flow past simple bodies using axial sourcesand a least-squares methodJournal of Aircraft, 1984