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: Monograph (Technical Report)
Uncontrolled Keywords: Aircraft design;Light aircraft;Loads
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Users 64 not found.
Date Deposited: 16 Jun 2006
Last Modified: 24 May 2010 04:13

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