A simple cost related objective function for mdo of transport aircraft

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Giesing, Joseph P ^a   Wakayama, Sean ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CONCEPTUAL DESIGN; DESIGN AIDS; OPERATING COSTS; SENSITIVITY ANALYSIS; STRUCTURAL ANALYSIS; TRANSPORT AIRCRAFT;

BASELINE VALUES; COST DATA; DIRECT OPERATING COSTS; LOW FIDELITIES; MEDIUM RANGE; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OBJECTIVE FUNCTIONS; TAKE OFF GROSS WEIGHT;

COSTS;

EID: 84982318988     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Johnson, V. S. "Minimizing Life Cycle Cost for Subsonic Commercial Aircraft", Vol. 27, № 2, Journal of Aircraft. Feb. 1990.
2. Scott, P.W. "The Cost Effectiveness of Weight Reduction by Advanced Material Substitution" SAE Aerospace Technology Conf. and Exposition, Long Beach, Ca. Oct. - 1986.
3. Liebeck, R. H., et. al. "Advanced Subsonic Airplane Design & Economic Studies" NASA CR-195443, April 1995.
4. Wakayama, S., and Kroo, I., "Subsonic Wing Planform Design Using Multidisciplinary Optimization", Journal of Aircraft, Vol. 32, № 4, July-Aug. 1995, pp. 746-753.
5. Wakayama, S., Lifting Surface Design Using Multidisciplinary Optimization, Ph.D. Dissertation, Stanford University Department of Aeronautics and Astronautics, Stanford, Dec. 1994.
6. Wakayama, S., Page, M., and Liebeck, R., "Multidisciplinary Optimization on an Advanced Composite Wing," AIAA-96-4003, 1996.
7. Wakayama, S., and Kroo, I., "A Method for Lifting Surface Design Using Nonlinear Optimization", AIAA Paper 90-3290, Sept. 1990.