Multidisciplinary design optimization of a transonic commercial transport with a strut-braced wing

SAE Technical Papers

Volumn , Issue , 1999, Pages

  Gern, F H ^a   Gundlach, J F ^a   Ko, A ^a   Naghshineh Pour, A ^a   Sulaeman, E ^a   Tetrault, P A ^a   Grossman, B ^a   Kapania, R K ^a   Mason, W H ^a   Schetz, J A ^a   Haftka, R T ^b  

^a State University   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; COMPUTATIONAL FLUID DYNAMICS; DESIGN AIDS; NANOCANTILEVERS; NASA; STRUTS; SUPERSONIC AIRCRAFT;

AERODYNAMIC ANALYSIS; COMMERCIAL TRANSPORT; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; FLIGHT-OPTIMIZATION-SYSTEMS; MULTIDISCIPLINARY DESIGN OPTIMIZATION; MULTIDISCIPLINARY DESIGN TEAMS; REMAINING COMPONENT; WING CONFIGURATIONS;

AERODYNAMIC DRAG;

EID: 85072447934     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/1999-01-5621     Document Type: Conference Paper

References (22)

1. Pfenninger, W., "Design Considerations of Large Subsonic Long Range Transport Airplanes with Low Drag Boundary Layer Suction," Northrop Aircraft, Inc., Report NAI-54-800 (BLC-67), November 1954.
2. Gunston, B., Giants of the Sky: The Biggest Aeroplanes of All Time, Patrick Stephens Limited, Wellingborough, UK, pp. 240-250.
3. Kulfan, R.M., and Vachal, J.D., "Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes," Boeing Commercial Airplane Company, AFFDL-TR-78-16, February 1978.
4. Jobe, C.E., Kulfan, R.M., and Vachal, J.D., "Wing Planforms for Large Military Transports," AIAA-78- 1470, 1978.
5. Turriziani, R.V., Lovell, W.A., Martin, G.L., Price, J.E., Swanson, E.E., and Washburn, G.F., "Preliminary Design Characteristics of a Subsonic Business Jet Consept Employing an Aspect Ratio 25 Strut-Braced Wing," NASA CR-159361, October 1980.
6. Smith, P.M., DeYOung, J., Lovell, W.A., Price, J.E., and Washburn, G.F.,"A Study of High-Altitude Manned Research Aircraft Employing Strut-Braced Wings of High-Aspect Ratio," NASA CR-159262, February, 1981.
7. Grasmeyer, J.M., Naghshineh Pour, A., Tetrault, P.-A., Grossman, B., Haftka, R.T., Kapania, R.K., Mason, W.H., Schetz, J.A., Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft with Tip- Mounted Engines, MAD 98-01-01, 1998.
8. Grasmeyer, J.M., Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft, MS Thesis, Virginia Polytechnic Institute & State University, April 1998.
9. Martin, K.C., Kopec, B.A.,"A Structural and Aerodynamic Investigation of a Strut-Braced Wing Transport Aircraft Concept" NAS1-96014, November 1998.
10. Vanderplaats Research & Development, Inc., DOT User's Manual, Version 4.20, Colorado Springs, CO, 1995.
11. Gundlach, J.F., Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport, MAD 99-06-03, 1999
12. Hoerner, S.F., Fluid Dynamic Drag: Practical Information on Aerodynamic Drag and Hydrodynamic Resistance, published by Mrs. Hoerner, 1965. Current address: P.O. Box 65283, Vancouver, WA 98665.
13. Pirzadeh, S., "Structured Background Grids for Generation of Unstructured Grids by Advancing-Front Method" AIAA Journal, Vol. 31, February 1993, pp. 257-265. (Pubitemid 23640426)
14. Frink, N.T., Pirzadeh, S., and Parikh, P., "An Unstructured- Grid Software System for Solving Complex Aerodynamic Problems" NASA CP-3291, May 1995.
15. Frink, N.T., Parikh, P., and Pirzadeh, S., "A Fast Upwind Solver for the Euler Equations on Three- Dimensional Unstructured Meshes" AIAA-91-0102, 1991.
16. McCullers, L.A., FLOPS User's Guide, Release 5.81. Text file included with the FLOPS code.
17. Naghshineh-Pour, A.H., Kapania, R., Haftka, R., Preliminary Structural Analysis of a Strut-Braced Wing, VPI-AOE-256, June 1998.
18. Torenbeek, E., "Development and Application of a Comprehensive, Design Sensitive Weight Prediction Method for Wing Structures of Transport Category Aircraft," Delft University of Technology, Report LR- 693, Sept. 1992.
19. Roskam, J., Methods for Estimating Stability and Control Derivatives of Conventional Subsonic Airplanes, Roskam Aviation and Engineering Corp., Lawrence, KS, 1971.
20. Grasmeyer, J.M., Stability and Control Derivative Estimation and Engine-Out Analysis, VPI-AOE-254, January 1998.
21. Mattingly, J.D., Heiser, W.H., and Daley, D.H., Aircraft Engine Design, AIAA, Washington, D.C., 1987.
22. Roskam, J., and Lan, C.-T.E., Airplane Aerodynamics and Performance, DARCorporation, Lawrence, KS, 1997.