Comparison of Aircraft Conceptual Design Weight Estimation Methods to the Flight Optimization System

Horvath, Bryce L ; Wells, Douglas P

关键词: AIRCRAFT DESIGN;    DESIGN ANALYSIS;    FLIGHT OPTIMIZATION;    STRUCTURAL WEIGHT;    SYSTEMS ANALYSIS;    COST ESTIMATES;    ESTIMATING;    MODULES;    SPACE EXPLORATION;   

RP-ID  :  NF1676L-27388

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Weight estimation is critical in the aircraft conceptual design process. The Flight Optimization System (FLOPS) is an aircraft conceptual design tool that has been the primary aircraft synthesis software used by the Systems Analysis and Concepts Directorate at NASA Langley Research Center. FLOPS includes multiple modules that represent aircraft design disciplines. The FLOPS weight module includes estimation methods that are similar in nature to other regression based aircraft preliminary weight estimation methods, however the FLOPS methods were created to use a minimum number of input parameters to limit the effort required by the designer to apply it. As FLOPS has recently been made publically available, this work compares the FLOPS weight estimation methods with several similar methods with the goal of explaining the differences in FLOPS, providing conceptual designers with a brief introduction to the method before attempting to apply it, and providing a reference to inform the development of future weight estimating relationships. In this paper, the Boeing 737-200 is used as a test case to highlight to differences and similarities in the methods.