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Aravind, and Somenath, Mukharjee (2005) A Theoretical Formulation For Flutter Analysis Of A Typical Subsonic Aircraft Wing (SARAS) Using Quasi-steady Aerodynamic Theory. Project Report. National Aerospace Laboratories, Bangalore.
Adiga, BS and Muralidhar, SJ and Ramesh, C and Aravind, (1991) PC based A 320 quick access recorder readout facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.