Noisy aerodynamic response and smooth approximations in HSCT design

5th Symposium on Multidisciplinary Analysis and Optimization, 1994

Volumn , Issue , 1994, Pages 1117-1128

  Giunta, Anthony A ^a,b   Dudley, Jane M ^a,b   Narducci, Robert ^a,b   Grossman, Bernard ^a,b   Haftka, Raphael T ^a,b   Mason, William H ^a,b   Watson, Layne T ^a,c  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Aerospace and Ocean Engineering   (United States)

^c Octorara Area High School   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DRAG; FIGHTER AIRCRAFT; STRUCTURAL OPTIMIZATION; SURFACE PROPERTIES;

CONVERGENCE DIFFICULTY; CONVERGENCE PROBLEMS; HIGH SPEED CIVIL TRANSPORTS; POLYNOMIAL FUNCTIONS; RESPONSE SURFACE METHOD; RESPONSE SURFACE TECHNIQUES; SEQUENTIAL APPROXIMATE OPTIMIZATION; SMOOTH APPROXIMATION;

AERODYNAMIC DRAG;

EID: 33847521077     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Unger, E. R., Hutchison, M. G., Rais-Rohani, M., Haftka, R. T., and Grossman, B., “Variable-Complexity Design of a Transport Wing,” Intl. J. Systems Automation: Res. and Appl. (SARA), No. 2, pp. 87-113.
2. Hutchison, M. G., Huang, X.-M., Mason, W. H., Haftka, R. T., and Grossman, B., “Variable-Complexity Aerodynamic-Structural Design of a High-Speed Civil Transport Wing,” AIAA Paper 92-4695, Sept. 1992.
3. Hutchison, M. G., Unger, E. R., Mason, W. H., Grossman, B., and Haftka, R. T., “Variable-Complexity Aerodynamic Optimization of an HSCT Wing Using Structural Wing-Weight Equations,” J. Aircraft, vol. 31, No. 1, 1994, pp. 110-116.
4. Hutchison, M. G., Unger, E. R., Mason, W. H., Grossman, B., and Haftka, R. T., “Aerodynamic Optimization of an HSCT Wing Using Variable- Complexity Modeling,” AIAA Paper 93-0101, Jan. 1993.
5. Healy, M. J., Kowalik, J. S, and Ransay, J. W., “Airplane Engine Selection by Optimization on Surface Fit Approximations,” J. Aircraft, vol. 12, No. 7, 1975, pp. 593-599.
6. Engelund, W. C., Stanley, D. O., Lepsch, R. A., McMillian, M. M., and Unal, R., “Aerodynamic Configuration Design Using Response Surface Methodology Analysis,” AIAA Paper 93-3967, Aug. 1993.
7. Hutchison, M. G., “Multidisciplinary Optimization of High-Speed Civil Transport Configurations Using Variable-Complexity Modeling,” Ph.D. Dissertation, VPI&SU, March 1993.
8. Craidon, C. B., “Description of a Digital Computer Program for Airplane Configuration Plots,” NASA TM X-2074, 1970.
9. Harris, R. V., Jr., “An Analysis and Correlation of Aircraft Wave Drag,” NASA TM X-947, 1964.
10. Carlson, H. W., and Miller, D. S., “Numerical Methods for the Design and Analysis of Wings at Supersonic Speeds,” NASA TN D-7713, 1974.
11. Carlson, H. W., and Mack, R. J., “Estimation of Leading-Edge Thrust for Supersonic Wings of Arbitrary Planforms,” NASA TP-1270, 1978.
12. Carlson, H. W., Mack, R. J., and Barger, R. L., “Estimation of Attainable Leading-Edge Thrust for Wings at Subsonic and Supersonic Speeds,” NASA TP-1500, 1979.
13. Grandhi, R. V., Thareja, R., and Haftka, R. T., “NEWSUMT-A: A General Purpose Program for Constrained Optimization Using Constraint Approximation,” ASME J. Mechanisms, Transmissions and Automation in Design, vol. 107, 1985, pp. 94-99.
14. Joh, C.-Y., Grossman, B., and Haftka, R. T., “Design Optimization of Transonic Airfoils,” Eng. Opt, vol. 21, No. 1, 1993, pp. 1-20.
15. Narducci, R., Grossman, B., and Haftka, R. T., “Sensitivity Algorithms for an Inverse Design Problem Involving a Shock Wave,” AIAA Paper 94-0096, Jan. 1994.
16. Khuri, A. I., and Cornell, J. A., Response Surfaces: Designs and Analyses, Marcel Dekker, Inc., New York, N. Y., 1987.
17. TX| Criterion, and Some Related Matters,” Technometrics, vol. 13, No. 4, 1971, pp. 731-742.
18. Furuya, H. and Haftka, R. T., “Locating Actuators for Vibration Suppression on Space Trusses by Genetic Algorithms,” ASME Winter Annual Meeting, 1993.
19. Mason, R. L., Gunst, R. F., and Hess, J. L., Statistical Design and Analysis of Experiments, John Wiley & Sons, New York, N. Y., 1989, pp. 215-221.