Numerical simulation of aerodynamic interactions among helicopter rotor, fuselage, engine and body of revolution
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-014-5545-x.pdf
Reference22 articles.
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2. Richard E B, Andrew J L. Efficient high-resolution wake modeling using the vorticity transport equation. AIAA J, 2005, 43: 1434–1443
3. Massimo G, Giovanni B. Novel boundary integral formulation for blade-vortex interaction aerodynamics of helicopter rotors. AIAA J, 2007, 45: 1169–1176
4. Steijl R, Barakos G N. Sliding mesh algorithm for CFD analysis of helicopter rotor-fuselage aerodynamics. Inte J Numer Methods Fluids, 2008, 58: 527–549
5. Steijl R, Barakos G N. Computational study of helicopter rotor-fuselage aerodynamic interactions. AIAA J, 2009, 47: 2143–2157
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