Dwarakanath, GS and Ramamoorthy, P and Rao, DM (1974) Evaluation of the transonic wave drag integral with particular reference to a real aircraft. Technical Report. National Aeronautical Laboratory, Bangalore,India.
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Abstract
The motivation for work on the wave drag integral was to carry out area ruling studies on an existing combat aircraft configuration. It is necessary (for discussion later on) to briefly recall the salient points. in the derivation of the wave drag integral.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Wave drag integral;Combat Aircraft Configuration |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics, Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 14 Sep 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2719 |
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