Aeroprediction: Difference between revisions
wikademia>Headbomb →References: remove references, these are lists of articles that used the program, which doesn't tell anyone a thing about the program itself |
wikademia>Dr. Fresh |
||
| (4 intermediate revisions by 4 users not shown) | |||
| Line 1: | Line 1: | ||
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. | |||
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.{{ | |||
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.{{ | 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}} | ||
==See also== | ==See also== | ||
*[[Missile Datcom]] | *[[Missile Datcom]] | ||
==References== | |||
[[Category:Aerospace engineering]] | [[Category:Aerospace engineering]] | ||
[[Category:Aerodynamics]] | [[Category:Aerodynamics]] | ||
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.