Three dimensional rectangular wing morphed to prevent stall and operate at design local two dimensional lift coefficient

Author:

Roy AritrasORCID,Mukherjee RinkuORCID

Funder

Defence Research and Development Organisation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Aerodynamic flight test results for the adaptive compliant trailing edge;Cumming,2016

2. The x-53 a summary of the active aeroelastic wing flight research program;Pendleton,2007

3. Optimized design of an active extrados structure for an experimental morphing laminar wing;Coutu;Aerosp. Sci. Technol.,2010

4. Aero-structural optimization and performance evaluation of a morphing wing with variable span and camber;Vale;J. Intell. Mater. Syst. Struct.,2011

5. A review of morphing aircraft;Barbarino;J. Intell. Mater. Syst. Struct.,2011

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