Evaluation of the Impacts of Objective Function Definition in Aircraft Conceptual Design

被引:4
作者
Di Bianchi, Davi H. B. [1 ]
Orra, Tarik H. [1 ]
Silvestre, Flavio J. [2 ]
机构
[1] Technol Inst Aeronaut, Aeronaut Engn Dept, BR-12228900 Sao Jose Dos Campos, Brazil
[2] Technol Inst Aeronaut, Aeronaut Engn Div, BR-12228900 Sao Jose Dos Campos, Brazil
来源
JOURNAL OF AIRCRAFT | 2018年 / 55卷 / 03期
关键词
OPTIMIZATION;
D O I
10.2514/1.C034277
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a successive derivation of basic equations in order to enlighten the implicit relationships between some of the most common objective functions employed in aircraft conceptual design. Correlation between financial and technical figures of merit relies on some important assumptions that may breakdown under certain circumstances, and therefore it is ill-advised to look for financially optimal designs using technical objective functions. As shown in the Results section, relationships between technical-only figures of merit hold and their behavior is even mathematically predictable. On the other hand, technical-financial relationships depend on market variables (price and market forecast, mainly) that can be captured only by proper market and financial models. In the Results section it is shown how optimization using technical-only objective functions overlooks important economical trades and thereby emphasizes the need for a proper modeling of such disciplines within the multidisciplinary analysis and optimization framework.
引用
收藏
页码:1231 / 1243
页数:13
相关论文
共 23 条
[1]  
[Anonymous], 2003006 ESTECO
[2]  
Bianchi D. H. B., AV TECHN INT OP C AI, DOI [10. 2514/6. 2015-2737, DOI 10.2514/6.2015-2737]
[3]  
BIRKLER JL, 1982, N1882AF RAND CORP
[4]  
Eastlake C. N., 2000, ASEE ANN C EMBR RIDD
[5]  
Giesing J. P., 35 AIAA AER SCI M EX, DOI [10. 2514/6. 1997-356, DOI 10.2514/6.1997-356]
[6]  
Gudmundsson S, 2014, GENERAL AVIATION AIRCRAFT DESIGN: APPLIED METHODS AND PROCEDURES, P661, DOI 10.1016/B978-0-12-397308-5.00015-5
[7]  
Hess R.W., 1987, R3255AF RAND CORP R3255AF RAND CORP
[8]  
Isikveren A., 2003, AER C EXH SAE INT MO, V112, P699, DOI [10.4271/2003-01-3063, DOI 10.4271/2003-01-3063]
[9]   MINIMIZING LIFE-CYCLE COST FOR SUBSONIC COMMERCIAL AIRCRAFT [J].
JOHNSON, VS .
JOURNAL OF AIRCRAFT, 1990, 27 (02) :139-145
[10]   Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration [J].
Kenway, Gaetan K. W. ;
Martins, Joaquim R. R. A. .
JOURNAL OF AIRCRAFT, 2014, 51 (01) :144-160