Memorandum report BRL-MR-
3870. Ballistic research laboratory, Aberdeen Proving Ground, Maryland, 1990, - 34 p.A method is presented for determining the Magnus force coefficient for use with the Modified Point Mass Trajectory model, to improve the simulated the of flight, based on the firing table experimental range firing impact and time-of-flight data. A comparison is made with the Magnus force coefficients determined from aerodynamic force for the 155mm, HE, M107 and 8-Inch, HE, RA, M650 projectiles. The Magnus force coefficients contained in the firing table data base for artillery projectiles are presented.Contents:
Introduction.
Discussion and Result.
Conclusions.
