Seshadri, SN (1993) Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds. Technical Report. NAL, Bangalore.
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Abstract
A Computer Code Has Been Developed To Predict The Drag Characteristics Of Missile Configurations At Subsonic, Transonic And Supersonic Speeds And Is Based On Semi-Empirical Methods . The Method' Handles Complex Configurations (Wing, Body, Tail, Canard) And Is Valid Upto High Angles Of Attack . The Code Has Been Validated Against A Large Number Of Experimental Results Particularly At Supersonic Speeds . The Agreement Between Prediction And Experiment Is Very Good . Validation At Subsonic And Transonic Speeds Is In Progress .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Missile Drag; Drag Characteristics |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Division/Department: | Experimental Aerodynamics Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 08 Aug 2012 15:30 |
| Last Modified: | 08 Aug 2012 15:30 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10766 |
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