Seshadri, SN (1993) Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds. Technical Report. NAL, Bangalore.
![]() |
PDF
pd_ea_9303.pdf Download (55kB) |
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: | Monograph (Technical Report) |
---|---|
Uncontrolled Keywords: | Missile Drag; Drag Characteristics |
Subjects: | ASTRONAUTICS > Astronautics (General) |
Depositing User: | M/S ICAST NAL |
Date Deposited: | 08 Aug 2012 10:00 |
Last Modified: | 08 Aug 2012 10:00 |
URI: | http://nal-ir.nal.res.in/id/eprint/10766 |
Actions (login required)
![]() |
View Item |