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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