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The '''Aeroprediction''' Code is a semi-empirical [[computer program]] that estimates the [[aerodynamics]] of weapons over the Mach number range 0 to 20, angle of attack range 0 to 90 degrees and for configurations that have various cross sectional body shapes. Weapons considered include [[projectiles]], [[missiles]], [[bombs]], [[rockets]] and [[Mortar (weapon)|mortars]]. Both static and dynamic aerodynamics are predicted with good accuracy.{{Citation needed|date=August 2009}} The code also predicts the trajectory of the weapon using the aerodynamics predicted by the code.
'''Aeroprediction'''   The Aeroprediction Code is a semi-empirical [[computer program]] that estimates the [[aerodynamics]] of weapons over the Mach number range 0 to 20, angle of attack range 0 to 90 degrees and for configurations that have various cross sectional body shapes. Weapons considered include [[projectiles]], [[missiles]], [[bombs]], [[rockets]] and [[mortars]]. Both static and dynamic aerodynamics are predicted with good accuracy. The code also predicts the trajectory of the weapon using the aerodynamics predicted by the code. The code can be purchased through Aeropredition, Inc.(email: drfgmoore@ hotmail.com)


The code may be used to compute the [[center of pressure]] and [[static margin]] of missiles.
The code may be used to compute the [[center of pressure]] and [[static margin]] of missiles.
The [[Defense Acquisition Workforce Improvement Act]] provides insights into how to use aerodynamic prediction codes such as Aeroprediction in the design of missile for US acquisition.


==References==
The [[Defense Acquisition Workforce Improvement Act]] provides insights into how to use aerodynamic prediction codes such as Aeroprediction in the design of missile for US acquisition.{{Citation needed|date=August 2009}}
*Moore, F.G., Approximate Methods for Weapon Aerodynamics, AIAA Progress in Astronatuics and Aeronautics, Volume 186
* Thomas Sooy, T., Schmidt, R., ''Aerodynamic Predictions, Comparisons, and Validations Using Missile Datcom and Aeroprediction 98 (AP98)'', 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 5-8, 2004


==See also==
==See also==
*[[Missile Datcom]]
*[[Missile Datcom]]
==References==


[[Category:Aerospace engineering]]
[[Category:Aerospace engineering]]
[[Category:Aerodynamics]]
[[Category:Aerodynamics]]
{{simulation-software-stub}}

Latest revision as of 11:26, 18 November 2010

The Aeroprediction Code is a semi-empirical computer program that estimates the aerodynamics of weapons over the Mach number range 0 to 20, angle of attack range 0 to 90 degrees and for configurations that have various cross sectional body shapes. Weapons considered include projectiles, missiles, bombs, rockets and mortars. Both static and dynamic aerodynamics are predicted with good accuracy. The code also predicts the trajectory of the weapon using the aerodynamics predicted by the code.

The code may be used to compute the center of pressure and static margin of missiles.

The Defense Acquisition Workforce Improvement Act provides insights into how to use aerodynamic prediction codes such as Aeroprediction in the design of missile for US acquisition.

See also

References