Download M47 Patton by Robert J. Icks PDF

By Robert J. Icks

Изображения: черно-белые фото,цветные рисунки

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Example text

Clp: Roll damping aerodynamic coefficient. Cldd: Fin cant aerodynamic coefficient. Cmq: Pitch damping moment aerodynamic coefficient. Dcop: Distance from the mass center to the center of pressure. Dmag: Distance from the mass center to the center of Magnus. CFD: Computational Fluid Dynamics. References [1] [2] [3] [4] [5] J. Sun, R. Cummings, “Evaluation of Missile Aerodynamic Characteristics Using Rapid Prediction Techniques,” Journal of Spacecraft and Rockets, Vol 21, No 6, pp 513-520, 1984. F.

8 s. ψ(°) γ (°) ∆y (mm) ∆z (mm) Table 4: 29 90 0÷360 0 +920 0 0 0 -14(-17) 0 90 +920 0 0 180 0 +14(+17) 0 270 -920 0 Uphill fire Coriolis deflections, calculated numerically and analytically (deviating analytical results in brackets). 8 s. 4 Example 4 The same data are used as in example 3, however the elevation angle changes to φ0 = 47° and the latitude to ψ = 45°. 03 m, which is slightly longer than in example 3, although gravity pulls the projectile back. The reason is the decreasing air pressure along the trajectory.

A. E. Anderson, WIT Press 2005. , Analytical calculation of trajectories using a power law for the drag coefficient variation with Mach number. Computational Ballistics II, pp. 303 – 312, Eds. V. A. A. E. Anderson, WIT Press 2005. , Verfahren zur nachträglichen Berücksichtigung von CoriolisEffekten bei der Bestimmung der Flugbahnen von Geschossen, unpublished report, Hamburg, 2005. , Thermodynamic and Transport Properties of Fluids, Basil Blackwell Ltd. Oxford, 4th Edition, 1988. , Einführung in die Technische Mechanik, 3.

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