Robust Structural Design for Active Aeroelastic Wing with Aerodynamic Uncertainties

Presented at the 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Atlanta, GA, April 3-6, 2000.

[1]  Dimitri N. Mavris,et al.  Maneuver Trim Optimization Techniques for Active Aeroelastic Wings , 2000 .

[2]  Daniel P. Schrage,et al.  System Synthesis in Preliminary Aircraft Design Using Statistical Methods , 1996 .

[3]  Dimitri N. Mavris,et al.  Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing , 1998 .

[4]  Robert Ryan,et al.  X-29A aircraft structural loads flight testing , 1989 .

[5]  Richard J. Beckman,et al.  A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output From a Computer Code , 2000, Technometrics.

[6]  M. Love,et al.  An ASTROS application with path dependent results , 1996 .

[7]  T. Cruse,et al.  Advanced probabilistic structural analysis method for implicit performance functions , 1990 .

[8]  Daniella E. Raveh,et al.  Structural Optimization of Flight Vehicles with Computational-Fluid-Dynamics-Based Maneuver Loads , 1999 .

[9]  Lockheed Martin,et al.  STRUCTURAL OPTIMIZATION WITH STRESS AND AEROELASTIC CONSTRAINTS USING EXPANDABLE MODAL BASIS , 1998 .

[10]  G. Miller An active flexible wing multi-disciplinary design optimization method , 1994 .

[11]  M. Love,et al.  ENHANCED MANEUVER AIRLOADS SIMULATION FOR THE AUTOMATED STRUCTURAL OPTIMIZATION SYSTEM - ASTROS* , 1997 .

[12]  Asme,et al.  A collection of technical papers : 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 15-17, 1996, Salt Lake City, UT , 1996 .

[13]  J. Volk,et al.  Integration of a generic flight control system into ASTROS , 1996 .

[14]  M. Karpel,et al.  Modal-Based Structural Optimization with Static Aeroelastic and Stress Constraints , 1996 .

[15]  L Krist Sherrie,et al.  CFL3D User''s Manual (Version 5.0) , 1998 .

[16]  Daniella E. Raveh,et al.  Nonlinear Design Loads for Maneuvering Elastic Aircraft , 2000 .

[17]  Douglas C. Montgomery,et al.  Response Surface Methodology: Process and Product Optimization Using Designed Experiments , 1995 .

[18]  Gerald D Miller Active Flexible Wing (AFW) Technology , 1988 .

[19]  C. F. Chen,et al.  The use of finite element methods for predicting the aerodynamics of wing-body combinations , 1970 .

[20]  Michael Kehoe,et al.  A flight research program for active aeroelastic wing technology , 1996 .

[21]  D. J. Neill,et al.  ASTROS - A multidisciplinary automated structural design tool , 1987 .

[22]  W. P. Rodden,et al.  Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics , 1985 .