The method of determination of aerodynamic resistance of aviation munitions is developed on attack aircraft. In basis of the developed method the mathematical design of the gas-dynamic flowing around of different aviation munitions with the use of heuristic and retrospective methods, and similarly experimental information. Presented grid models of the system a "airframe – power-plant – aviation munitions" for the use in solvere of programmatic complex. Verification of method it is conducted by comparing results of calculation with the known experimental information.
battle airplane, attack aircraft, airplane, aviation munitions, coefficient of aerodynamic resistance, technical flight characteristics