Aerospace Science and Technology 14 (2010) 1–10 Contents lists available at ScienceDirect Aerospace Science and Technology www.elsevier.com/locate/aescte Propulsion and…
THE FINITE WING 9.1. The Finite Wing. TTp to this point we have considered only two- tlimensional flow and have carried that development up to its current stabus as a coherent…
Journal of Sound and Vibration (1988) 123(1), 1-13 ANALYSIS OF LIMIT CYCLE FLUTTER OF AN AIRFOIL INCOMPRESSIBLE FLOW Z. C. YANG AND L. C. ZHAO Department of Aircraft Engineering,…