Iteration schemes for rapid post-stall aerodynamic prediction of wings using a decambering approach

Author:

Paul R. C.1,Gopalarathnam A.1

Affiliation:

1. Department of Mechanical and Aerospace Engineering; North Carolina State University; Raleigh NC 27695 USA

Funder

DoD SMART Scholarship

National Science Foundation GRFP

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference39 articles.

1. Laminar Research X-Plane http://www.x-plane.com

2. Inertiasoft, Inc FS One http://www.fsone.com

3. Selig MS Modeling full-envelope aerodynamics of small UAVs in realtime Virginia, USA 2010

4. Bunge RA Kroo IM Compact formulation of nonlinear inviscid aerodynamics for fixed-wing aircraft Virginia, USA June 2012

5. Tani I A simple method of calculating the induced velocity of a monoplane wing. Rep. No. 111 (vol. IX, p. 3) 1934

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