A status report is given on the development of PROGRAM MISSILE, which is a comprehensive aerodynamic prediction code capable of computing the longitudinal and lateral stability and control characteristics of cruciform body-tail and canard (wing)-body-tail tactical missiles. The methodology used is described and the planned data base extension is outlined. The rational modeling concepts used to extend the fin-body data base to general body-tail and canard-body-tail missiles are presented. (Author)
Status Report on Triservice Data Base Extension of Program Missile
1981
9 pages
Report
No indication
English
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