Higher level design methods applied to the conceptual design of an MALE UAV

12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, MAO

Volumn , Issue , 2008, Pages

  Iqbal, Liaquat U ^a   Crossley, William A ^a   Weisshaar, Terrence A ^a   Sullivan, John P ^a  

^a Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT DESIGN; AIRCRAFT GEOMETRIES; BLOCK DIAGRAMS; CAD MODELING; CAD/CAE; CONCEPT GENERATION; CRITICAL PARAMETER; DESIGN COMMUNITY; DESIGN CONCEPT; DESIGN METHOD; DESIGN PROCESS; EMPIRICAL FORMULAS; FUNCTIONAL FLOW; GEOMETRY PARAMETER; HAND-DRAWN SKETCHES; HIGH FIDELITY; LEVEL DESIGN; MATRIX; MEDIUM ALTITUDE LONG ENDURANCES; MS EXCEL; PLANFORM; QUANTITATIVE ANALYSIS; SELECTION METHODS; SIMPLIFIED CALCULATIONS; STRUCTURED DESIGN METHOD; WING PLANFORMS;

COMPUTER AIDED ANALYSIS; COMPUTER AIDED MANUFACTURING; CONCEPTUAL DESIGN; DRAWING (GRAPHICS); HAND TOOLS; OPTIMIZATION; PLANFORMS; PRODUCT DESIGN; QUALITY FUNCTION DEPLOYMENT; STRUCTURAL ANALYSIS; SWEPT WINGS;

COMPUTER AIDED DESIGN;

EID: 78049518687     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Peters C., Roth B., Crossley W. and Weisshaar T., "Use of Design Methods to Generate and Develop Missions for Morphing Aircraft" 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, Sep. 4-6, 2002 AIAA-2002-5468.
2. Taylor R. M., and Weisshaar T., "A. Merging computational structural tools into multidisciplinary team-based design" AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 8th, Long Beach, CA, Sept. 6-8, 2000 AIAA-2000-4820.
3. Taylor R. M., Weisshaar T., and Sarukhanov V., "Structural design progress improvement using evolutionary finite element models" AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 42nd, Seattle, WA, Apr. 16-19, 2001 AIAA-2001-1630.
4. Taylor R. M., Weisshaar T., and Sarukhanov V., "Structural Design Process Improvement Using Evolutionary Finite Element Models" Journal of Aircraft, Vol.43 No.1, 2006 pp.172-181.
5. Iqbal, L. U., Sullivan, J. P., "Integrated Suite for the Aircraft Design Integration, Optimization and Manufacturing", Proceedings of the International Conference on Comprehensive Product Realization (ICCPR), June 18-20, 2007, Beihang.
6. Iqbal, L. U., Sullivan, J. P., "Application of an Integrated Approach to the UAV Conceptual Design", Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA, Reno, Nevada, Jan. 7-10, 2008.
7. Pugh, S., "Conceptual Design," Total Design: Integrated Methods for Successful Product Engineering, Addison-Wesley, 1991, pp. 67-100.
8. Raymer, D. P., Aircraft Design: A Conceptual Approach, Fourth Edition, AIAA Education Series, 2004.
9. Brandt, et al, "Constraint Analysis: Designing to a Requirement," section 5.15, Introduction to Aeronautics, AIAA, Reston, VA, 1997, pp. 197-203.
10. Ullman, D. G., "Understanding the Problem and the Development of Engineering Specifications", The Mechanical Design Process, Third Edition, McGraw-Hill, 2003, pp. 111-135.
11. Blanchard, B. S. and Fabrycky, W. J., "Functional Analysis and Allocation", Systems Engineering and Analysis, Fourth Edition, Prentice Hall, Upper Saddle River, NJ, 2006, p. 78-85.
12. ANSYS Academic Teaching Advanced, Software Package, Ver. 11., ANSYS Inc. 02855 Telegraph Avenue, Suite 501, Berkeley, CA 94705.
13. CMARC/POSTMARC, Panel Code, Software Package, Ver. 6.4.1, Aerologic Inc. 1613 Altivo Way Los Angeles, CA 90026-2025.
14. FLUENT, CFD Package, Software Package, Ver. 6.3, Fluent Inc. 10 Cavendish Court, Lebanon, NH 03766.
15. CATIA, CAD Package, Ver. 5, IBM Corporation, 1 New Orchard Road Armonk, New York 10504-1722.
16. U.S. Air Force Fact Sheet MQ-1 PREDATOR, http://www.af.mil/factsheets/ factsheet-print.asp?fsID=122&page=1.
17. MATLAB R2008a, The MathWorks, Inc. Crystal Glen Office Centre 39555 Orchard Hill Place Suite 280, Novi, MI 48375.