Design of the main landing gear for the NALLA prototype

Damania, RB and Karthik, K and Kumar, Mahesh and Aravamudhan, Srikanth (1991) Design of the main landing gear for the NALLA prototype. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    This report documents the design of the main landing gear for NAL's light aircraft. The federwal aviation regulations (FAR), Part 23, were used to estimate loads. The gear was designed from deflection and stress criteria. Factors influencing the design are listed along with the results of all calculations

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Landing gear design;Light airplane;Cantilever spring
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Mr. N A
    Date Deposited: 29 Jun 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1761

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