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aerodynamic aeroelastic aircraft airfoil airplane alkanes analysis angle of attack applied assumed axial boundary conditions calculated canard cell coefficient configuration constant corrosion cost curve cylinder delta wing developed displacement drag drag coefficient dynamic effect elastic energy Engineering equations experimental finite element finite element method flight flow force fracture fracture mechanics frequency fuel function given heat horizontal increase initial integral Israel Israel Journal iteration kerogen leading edge lift linear Mach number maximum mechanics method mode NASA nondimensional nonlinear obtained oil shale ONERA operation optimal control paper parameters plane plate predicted present pressure problem radiation ratio reaction reactor reduced rotating shale shell shown in Fig simulation slender wing solar solution speed stability stiffened stress intensity factors structure subsonic supersonic surface Table Technion Technology temperature theory thermal tion trailing edge trajectories transonic variable velocity vibration vortex vortex lift vortices