Multi-disciplinary analysis and optimization applied to supersonic aircraft part 2: Application & results

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 2, Issue , 2007, Pages 1862-1876

  Herrmann, U ^a,c   Laban, M ^b,d  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^c Transport Aircraft Branch   (Germany)

^d NLR   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC FIDELITY; FLIGHT MISSION; MULTI-DISCIPLINARY ANALYSIS; SUPERSONIC TRANSPORT AIRCRAFTS;

CONCEPTUAL DESIGN; OPTIMIZATION; PARAMETER ESTIMATION; SUPERSONIC AERODYNAMICS; WINGS;

AIRCRAFT;

EID: 34547502361     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Herrmann, U., "Designing High-Lift Systems for Low Drag: SCT", Von Karman Institute Lecture Series hosted by the National Institute of Aerospace: CFD-based Aircraft Drag Prediction and Reduction, Hampton, USA, November 3rd - 7th, 2003.
2. Herrmann, U., "Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft", Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag, Germany, 2006.
3. Herrmann, U., "CISAP: Cruise Speed Impact on Supersonic Aircraft Planform - a Project Overview", AIAA 2004-4539, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York, 2004.
4. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2005.
5. Laban, M., "Multi-Disciplinary Analysis and Optimization of Supersonic Transport Aircraft Wing Planforms", AIAA 2004-4542, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York, 2004.
6. Laban, M., Herrmann, U., "Multi-Disciplinary Analysis and Optimisation Applied to Supersonic Aircraft; Part 1 : Analysis Tools", AIAA 2007-1857, 3rd AIAA Multidisciplinary Design Optimization Specialist Conference, Honolulu, Hawaii, April 2007.
7. Brodersen, O., M. Hepperle, A. Ronzheimer, C-C. Rossow and B. Scheming, "The Parametric Grid Generation System MegaCads" In: Soni, B.K., J.F. Thompson, J. Häuser and P. Eisemann (Ed.): "5th International Conference on Numerical Grid Generation in Computational Field Simulation". National Science Foundation (NSF), 1996, pp. 3535-3562. http://www.megacads.dlr.de.
8. Kroll, N., C.-C. Rossow, K. Becker and F. Thiele, "MEGAFLOW-A Numerical Flow Simulation System", Aerospace Science Technology, Vol. 4, pp. 223-237, 2000.
9. MSCNASTRAN 2001 Quick Reference Guide, MSCSoftware Corporation, USA, 2002, www.mscsoftware.com.
10. Rowan, T. H., "Functional Stability Analysis Of Numerical Algorithms", Ph.D. Thesis, Department of Computer Sciences, University of Texas at Austin, USA, May 1990.
11. Torenbeek, E., Jesse, E., Laban, M., "Conceptual design of a Mach 1.6 European Commercial Transport", AIAA 2004-4541, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New York, 2004.
12. Herrmann, U., "Multiple Discipline Maximum Take-Off Weight Minimization for Supersonic Transport Aircraft", Paper accepted for publication in Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag, Germany, 2007.