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DARcorp Advanced Aircraft Analysis 2.5.1.53 飞机设计测试

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  • 更新时间:2009-06-15 20:15:34
  • 软件类型:国外软件
  • 软件大小:请和我们联系得知
  • 软件语言:英文
  • 软件授权:正式版
  • 软件类别:交通运输
  • 应用平台:具体软件,请联系我们得知

软件介绍

DARcorp Advanced Aircraft Analysis 2.5.1.53 飞机设计测试

Advanced Aircraft Analysis (AAA)应用于对数的多数的固定机翼设置中,可以让学生和对数的设计工程师们通过对性能的和成本的估算,然后从重量的估计中得到一个飞机的配置。它可以用于对飞机的初步设计,可以对新型和现在的飞机稳定性和控制能力做以分析。也可以用于小型飞机的设计,包括军用和运输机。 Advanced Aircraft Analysis (AAA) is the industry standard aircraft design, stability, and control analysis software. With installations in over 45 countries, AAA is being used by major aeronautical universities, aircraft manufacturers, and military organizations worldwide. AAA provides a powerful framework to support the iterative and non-unique process of aircraft preliminary design. The AAA program allows students and preliminary design engineers to rapidly evolve an aircraft configuration from early weight sizing through open loop and closed loop dynamic stability and sensitivity analysis, while working within regulatory and cost constraints. AAA is used for preliminary and Class II design of airplanes, stability and control analysis of new and existing airplanes. Class II design incorporates detailed weight & balance, aerodynamics, stability & control calculations including trim analysis and flying qualities used in conjunction with the preliminary design sequence. Class II design accounts for power plant installation, landing gear disposition and component locations on the airplane. Class II uses more sophisticated methods than Class I and requires more detail information of the airplane to be known. The accuracy of Class II is therefore greater than Class I methods. AAA can be used for all sizes of aircraft from small airplanes all the way up to military and transport airplanes. The program is designed to assist in the design learning process while reserving for the user the individual creative judgment which is essential to the process of airplane design. Advanced Aircraft Analysis (AAA) applies to most fixed wing configurations (civil and military aircraft) and allows design engineers to rapidly evolve an airplane configuration from weight sizing through detailed performance calculations and cost estimations. All applicable performance and flying quality regulations are available in the AAA program. This provides the designer with an instant appraisal of the status of the design relative to these regulations. The design methodology used in Advanced Aircraft Analysis (AAA) is based on Airplane Design I-VIII, Airplane Flight Dynamics and Automatic Flight Controls, Parts I and II, by Dr. Jan Roskam, and Airplane Aerodynamics and Performance, by Dr. C.T. Lan and Dr. Jan Roskam. AAA incorporates the methods, statistical databases, formulas and relevant illustrations and drawings from these references. Advanced Aircraft Analysis has: 274,659 lines of code 4,397 unique parameters 9,187 variables on all windows 2,623 output parameters 546 different series of calculations 490 different I/O windows 118 different plots 91 different tables

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