The aerodynamic loading on a number of rocket body-control surface combinations has been calculated using methods developed at the University of Tennessee Space Institute over the past five years. Variations in control surface planform, roll angle, control surface deflection or incorporation of elevons, are included. Compressibility is accounted for. Details of the digital computer program are included.
A Study of Various Slender and Non-Slender Fin-Body Combinations of Missile Configurations
1976
189 pages
Report
Keine Angabe
Englisch
Rockets , Aerodynamics , Artillery rockets , Fin stabilized ammunition , Fins , Slender bodies , Pressure distribution , Potential flow , Elevons , Aerodynamic control surfaces , Aerodynamic loading , Computer programs , FORTRAN , Fin body configurations , Cruciform fins , Sweptback fins , FORTRAN 4 programming language
Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations
Engineering Index Backfile | 1949
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