Optimization of an advanced business jet

Journal of Aircraft

Volumn 34, Issue 3, 1997, Pages 288-295

  Gallman, John W ^a,c,d,e   Kaul, Randy W ^b,e,f   Chandrasekharan, Reuben M ^b,e,f   Hinson, Michael L ^b,e,f  

^a NASA AMES RESEARCH CENTER   (United States)

^b BOMBARDIER AEROSPACE   (Canada)

^c High Speed Aerodynamics Branch   (United States)

^d RAYTHEON COMPANY   (United States)

^e AIAA   (United States)

^f Applied Aerodynamics ^*

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; COMPUTER AIDED DESIGN; COMPUTER SIMULATION; COMPUTER SOFTWARE; ERROR ANALYSIS; OPTIMIZATION; SENSITIVITY ANALYSIS; WINGS;

BUSINESS JET AIRCRAFTS; MACH NUMBER;

JET AIRCRAFT;

EID: 0031143072     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2197     Document Type: Article

References (20)

1. Chandrasekharan, R. M., Hawke, V. M., Hinson, M. L., Kennelly, R. A., Jr., and Madson, M. D., "Aerodynamic Tailoring of the Learjet Model 60 Wing," Society of Automotive Engineers, Paper 932534, Sept. 1993.
2. Shevell, R. S., Fundamentals of Flight, Prentice-Hall, Englewood Cliffs, NJ, 1983.
3. Torenbeek, E., Synthesis of Subsonic Airplane Design, Delft Univ. Press and Martinus-Nijhoff Publishers, The Netherlands, 1982.
4. Gallman, J. W., Kroo, I. M., and Smith, S. C., "Optimization of Joined-Wing Aircraft," Journal of Aircraft, Vol. 30, No. 6, 1993, pp. 897-905.
5. Axelson, J. A., "AEROX-Computer Program for Transonic Aircraft Aerodynamics to High Angles of Attack," NASA TMX 73208, Feb. 1977.
6. Bayan, R., and Shevell, R., "Development of a Method for Predicting the Drag Divergence Mach Number and the Compressibility Drag Due to Conventional and Supercritical Wings," Dept. of Aeronautics and Astronautics, SUDAAR 522, Stanford Univ., Stanford, CA, July 1980.
7. Von Kármán, T., "Turbulence and Skin Friction," Journal of the Aeronautical Sciences, Vol. 1, No. 1, 1934, pp. 1-20.
8. McGeer, T., and Shevell, R., "A Method for Estimating the Compressibility Drag of an Airplane," Dept. of Aeronautics and Astronautics, SUDAAR 535, Stanford Univ., Stanford, CA, Jan. 1983.
9. Hoak, D. E., and Fink, R. D. (eds.), "USAF Stability and Control DATCOM," Wright-Patterson AFB, OH, April 1978.
10. Furlong, G. C., and McHugh, J. G., "A Summary and Analysis of the Low-Speed Longitudinal Characteristics of Swept Wings at High Reynolds Number," National Advisory Committee for Aeronautics, Rept. 1339, 1957.
11. Beltramo, M. N., Trapp, D. L., Kimoto, B. W., and Marsh, D. P., "Parametric Study of Transport Aircraft Systems Cost and Weight," NASA, CR 151970, April 1977.
12. Gallman, J. W., and Kroo, I. M., "Structural Optimization for Joined-Wing Synthesis," Journal of Aircraft, Vol. 33, No. I, 1996, pp. 214-223.
13. Moore, M., and Samuels, J., "ACSYNT-Aircraft Synthesis Program-User's Manual," NASA Ames Research Center, Moffett Field, CA, Sept. 1990.
14. Maskew, B., "Program VSAERO, a Computer Program for Calculating the Nonlinear Characteristics of Arbitrary Configurations, Theory Document," NASA CR 4023, Sept. 1987.
15. Maskew, B., "Program VSAERO, a Computer Program for Calculating the Nonlinear Characteristics of Arbitrary Configurations, Users Manual," NASA, CR 166476, Dec. 1982.
16. Roskam, J., Airplane Design-Part I, Roskam Aviation and Engineering Corp., Ottawa, KS, 1985.
17. Gill, P. E., Murray, W., and Wright, M. H., Practical Optimization, Academic, New York, 1981.
18. Gill, P. E., Murray, W., Saunders, M. A., and Wright, M. H., "User's Guide for NPSOL (Version 4.0): A Fortran Package for Nonlinear Programming," Dept. of Operations Research, TR SOL 86-2, Stanford Univ., Stanford, CA, Jan. 1986.
19. Vanderplaats, G. N., "CONMIN-A FORTRAN Program for Constrained Function Minimization-User's Manual," NASA Ames Research Center, TMX 62282, Moffett Field, CA, Aug. 1973.
20. Vanderplaats, G. N., Numerical Optimization Techniques for Engineering Design: With Applications, McGraw-Hill, New York, 1984.