1. Evaluating the impact of morphing technologies on aircraft performance;Browman,2002
2. Realization of morphing wings: a multidisciplinary challenge;Vasista;J. Aircraft,2012
3. Variable wing camber control for civil transport aircraft;Hilibig,1984
4. R.F. Brissenden, A.R. Heath, D.W. Conner, M.L. Spearman (technical monitors), the Boeing Preliminary Design Department, Assessment of variable camber for application to transport aircraft, NASA Contractor Report CR-158930, National Aeronautics and Space Administration Langley Research Center, Hampton, VA, October, 1980.
5. The Wright Flyer: An Engineering Perspective,1987