Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds

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