Ramabhadran, S and Sridharan, R (1982) Computation of the aerodynamic characteristics of wings in linearised supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
For the solution of tbe linearised supersonic flow equation, an explicit numerical scheme is discussed. Using this formulation,the aerodynamic characteristics of finite finite wings are coaputed based on lifting surface theory. Some results of the study of wing-fusalage configurations using this metbod are also given.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Analogue technique;Numerical methods |
| Subjects: | AERONAUTICS > Aircraft Stability and Control AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 24 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2489 |
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