Calculation of the Aerodynamic Tail Loads for NALLA

Ashok, G (1991) Calculation of the Aerodynamic Tail Loads for NALLA. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    The aerodynamic loads on the tail surfaces for NALLA have been estimated using FAR part 23. The methods used and the results obtained are Presented.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aircraft design;Light aircraft;Loads
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Centre for Civil Aircraft Design and Development
    Depositing User: Mr. Ravikumar R
    Date Deposited: 16 Jun 2006
    Last Modified: 24 May 2010 09:43

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