Comprehensive aircraft preliminary design methodology applied to the design of MALE UAV

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Iqbal, Liaquat U ^a   Sullivan, John P ^a  

^a Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE DESIGN; AIRCRAFT DESIGN; AIRCRAFT PRELIMINARY DESIGN; BACK-OF-THE-ENVELOPE CALCULATIONS; CAD/CAE; CONCEPT GENERATION; DESIGN CONCEPT; DESIGN CYCLE-TIME; DESIGN DATA; DESIGN METHOD; DESIGN PHASIS; DESIGN PROCESS; DESIGN SYNTHESIS; HAND-DRAWN SKETCHES; HIGH FIDELITY; INTEGRATION OF CAD AND CAE; MATRIX; MEDIUM ALTITUDE LONG ENDURANCES; MISSION ANALYSIS; MS EXCEL; MULTI-DISCIPLINARY DESIGNS; NEW PRODUCT; PRELIMINARY DESIGN; PRELIMINARY DESIGN PHASE; PROBLEM DEFINITION; PROBLEM SPECIFICATION; PRODUCT DEFINITION; QUANTITATIVE ANALYSIS; SELECTION METHODS; SOLUTION SYNTHESIS; STRUCTURED DESIGN METHOD;

AEROSPACE ENGINEERING; AEROSPACE INDUSTRY; COMPUTATIONAL FLUID DYNAMICS; COMPUTER AIDED DESIGN; DRAWING (GRAPHICS); HAND TOOLS; QUALITY FUNCTION DEPLOYMENT; SPREADSHEETS;

PRODUCT DESIGN;

EID: 78549277166     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Raymer, D. P., "Enhancing Aircraft Conceptual Design Using Multidisciplinary Optimization", Doctoral Thesis, May 2002, Royal Institute of Technology, Stockholm Sweden.
2. Ullman D. G., "Understanding the Problem and the Development of Engineering Specifications," Chapter 6, The Mechanical Design Process, Third Edition, McGraw-Hill, 2003, pp. 111-135.
3. Hunter, M. R., and Van Landingham, R. D., "Listening to the Customer Using QFD," Quality Progress, Vol. 27, No. 4, Apr. 1994, pp. 55-59.
4. Pugh, S., "Conceptual Design," Total Design: Integrated Methods for Successful Product Engineering, Addison-Wesley, 1991, pp. 67-100.
5. 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.
6. 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.
7. 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.
8. Nickol C. Guynn M. D., Kohout, L. L., and Ozoroski T.A., "High Altitude Long Endurance Air Vehicle Analysis of Alternatives and Technology Requirements Development", 45th AIAA Aerospace Sciences Meeting and Exhibit, 8 - 11 January 2007, Reno, Nevada.
9. https://akss.dau.mil/dag/GuideBook/IG-c3.3.asp.
10. 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, China.
11. Iqbal, L. U., Sullivan, J. P., "Application of an Integrated Approach to the UAV Conceptual Design", Proceedings of the 46th AIAA Aero Sciences Meeting and Exhibit, AIAA, Reno, Nevada, Jan. 7-10, 2008.
12. CATIA V5, CAD Package, Ver. 5, IBM Corporation, 1 New Orchard Road Armonk, New York 10504-1722.
13. CMARC/POSTMARC, Panel Code, Software Package, Ver. 6.4.1, Aerologic Inc. 1613 Altivo Way Los Angeles, CA 90026-2025.
14. DWT Panel Code, Software Package, Ver. 6.4.1, Aerologic Inc. 1613 Altivo Way Los Angeles, CA 90026-2025.
15. FLUENT, CFD Package, Software Package, Ver. 6.3, Fluent Inc. 10 Cavendish Court, Lebanon, NH 03766.
16. GAMBIT, FLUENT CFD Package, Software Package, Ver. 6.3, Fluent Inc. 10 Cavendish Court, Lebanon, NH 03766.
17. ANSYS Academic Teaching Advanced, Software Package, Ver. 11., ANSYS Inc. 02855 Telegraph Avenue, Suite 501, Berkeley, CA 94705.
18. CATIA, SIMULIA, The Dassault Systèmes Rising Sun Mills, 166 Valley Street, Providence, RI 02909-2499.
19. Raymer, D. P., Aircraft Design: A Conceptual Approach, Fourth Edition, AIAA Education Series, 2004.
20. Brandt, et al, "Constraint Analysis: Designing to a Requirement," Introduction to Aeronautics, AIAA, Reston, VA, 1997, pp. 197-203.
21. MS Excel, Microsoft Corporation, One Microsoft Way, Redmond, WA 98052-6399.
22. U.S. Air Force Fact Sheet MQ-1 PREDATOR, http://www.af.mil/factsheets/ factsheet-print.asp?fsID=122&page=1.