Estimation of the aerodynamic normal force and static moment of a given class of flight vehicles is demonstrated with reference to AMCP 706-280, which in turn derives from the classic British work 'Wings'. By means of linearized algebraic reduction, a transmutation permits the designer to quickly evaluate the effects of variation on the flight system.
Algorithm for Estimating Aerodynamic Static Moments of Long Rod Penetrators at 2 Less than M Less than 5
1980
49 pages
Report
No indication
English
Ammunition, Explosives, & Pyrotechnics , Detonations, Explosion Effects, & Ballistics , Projectiles , Rods , Aerodynamic forces , Aeroballistics , Terminal ballistics , Gyroscopes , Yaw , Fin stabilized ammunition , Algorithms , Mathematical prediction , Supersonic flight , Long projectiles , Static moment , Desktop calculators , AMCP-706-280 , Design
Estimating and benchmarking Less-than-Truckload market rates
Online Contents | 2010
|Transportation Research Record | 2008
|Long-Haul Shipment Optimization for Less-Than-Truckload Carriers
Online Contents | 2009
|Long-Haul Shipment Optimization for Less-Than-Truckload Carriers
Transportation Research Record | 2009
|Prevention is less costly than cure
Engineering Index Backfile | 1928