Development of Experimental Techniques to determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Closure Report for AR & DB Project AE-0-154

Patil, SR and Ramaswamy, MA (1988) Development of Experimental Techniques to determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Closure Report for AR & DB Project AE-0-154. Project Report. National Aerospace Laboratories, Bangalore.

Full text available as:
[img] PDF
Download (64Kb)

    Abstract

    The details of teetering rotor model and the associated strain gauge balance and calibration fixtures have been presented. Hovering results for 1 .22 m diameter teetering rotor model evaluated experimentally have been compared with the simple blade element - momentum theory.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Helicopter rotor models;Rotor aerodynamic performance; Development of experimental techniques
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 30 Aug 2012 16:18
    Last Modified: 30 Aug 2012 16:18
    URI: http://nal-ir.nal.res.in/id/eprint/10868

    Actions (login required)

    View Item