The use of structural optimality criteria for aircraft conceptual design

41st Structures, Structural Dynamics, and Materials Conference and Exhibit

Volumn , Issue , 2000, Pages

  Danilin, Alexander I ^a   Weisshaar, Terrence A ^b  

^a SAMARA NATIONAL RESEARCH UNIVERSITY   (Russian Federation)

^b Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONCEPTUAL DESIGN; DEFLECTION (STRUCTURES); LIFT; STIFFNESS; STRUCTURAL DYNAMICS; SUPERSONIC AIRCRAFT;

AEROELASTIC CONSTRAINTS; AEROELASTIC CONTROL; AIRCRAFT CONCEPTUAL DESIGNS; EARLY DESIGN STAGES; GRADIENT-BASED OPTIMIZATION METHOD; OPTIMALITY CRITERIA; STRUCTURAL LOCATIONS; SUPERSONIC TRANSPORT;

AEROELASTICITY;

EID: 85086615127     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-1328     Document Type: Conference Paper

References (9)

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2. V. A. Komarov, "Design of Load-carrying Scheme of Airframe, " Actual Problems of Aircraft Science and Engineering, Machinostriene, Moscow, 1984 (in Russian).
3. L.A. McCullers, "Automated Design of Advanced Composite Structures, " Proceedings of the ASME Structural Optimization Symposium, AMD-Vol. 7, Nov. 1974, pp. 119-133.
4. Wilkinson, K. et al., "An Automated Procedure for Flutter and Strength Analysis and Optimization of Aerospace Vehicles, Vol. 1-Theory and Application, " AFFDL-TR-75-137, U.S.A.F. Flight Dynamics Laboratory, December 1975.
5. E.H. Johnson and V.B. Vcnkayya,. "Automated Structural Optimization System (ASTROS), " Vol 1 Theoretical Manuel, AFWAL TR-88-3028, Dec. 1988.
6. New World Vistas-Air and Space. Power for the 21th Century, Aircraft and Propulsion, A Report to the Secretary of the Air Force, December 1995.
7. th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Optimization, St. Louis, Mo., September 1998.
8. th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City Beach, Florida, Sept. 7-9, 1994, pp. 679-689.
9. Sensburg, O. and Tischler, V. "A Unique Design for a Diverging Flexible Vertical Tail, " NATO/RTO Meeting, Ottawa, Canada, October 1999.