All Stories

  1. Generic High-Speed Vehicle Configuration Modeling and Optimization
  2. Shape Continuum Sensitivity Analysis using ASTROS and CAPS
  3. Quadratic Multipoint Exponential Approximation for Optimization and Uncertainty Quantification
  4. Continuum shape sensitivity analysis for aeroelastic gust using an arbitrary lagrangian-eulerian reference frame
  5. Unsteady Aerodynamic Stabilization of the Dynamics of Hingeless Rotor Blades in Hover
  6. Continuum Shape Sensitivity Analysis for Aeroelastic Gust using an Arbitrary Lagrangian-Eulerian Reference Frame
  7. Electromagnetic Modeling of Large Phased Arrays of Structurally Embedded Waveguides
  8. A novel imaging technique for measuring kinematics of light-weight flexible structures
  9. Geometric parameterization of wing planform enables design of its optimal shape
  10. Two forms of continuum shape sensitivity method for fluid–structure interaction problems
  11. Convergence Study of Local Continuum Sensitivity Method Using Spatial Gradient Reconstruction
  12. Discrete Adjoint Formulation for Continuum Sensitivity Analysis
  13. A Variational Principle for Unsteady Compressible Flow
  14. Continuum Sensitivity Analysis for Aeroelastic Shape Optimization
  15. Nonlinear Aeroelastic Scaled-Model Design
  16. Multiobjective optimization using an adaptive weighting scheme
  17. Nonintrusive Continuum Sensitivity Analysis for Aerodynamic Shape Optimization
  18. Discrete Adjoint Formulation for Continuum Sensitivity Analysis
  19. Reliability Based Structural Design using Continuum Sensitivity Analysis
  20. Local continuum shape sensitivity with spatial gradient reconstruction for nonlinear analysis
  21. Nonlinear Aeroelastic-Scaled-Model Optimization Using Equivalent Static Loads
  22. Nonintrusive Continuum Sensitivity Analysis for Aerodynamic Shape Optimization
  23. Local continuum shape sensitivity with spatial gradient reconstruction
  24. Aeroelastic Shape Optimization of a Flapping Wing
  25. Integration of Geometric Sensitivity and Spatial Gradient Reconstruction for Aeroelastic Shape Optimization
  26. Equivalence of continuum and discrete analytic sensitivity methods for nonlinear differential equations
  27. Boundary velocity method for continuum shape sensitivity of nonlinear fluid–structure interaction problems
  28. Continuum Shape Sensitivity with Spatial Gradient Reconstruction of Built-up Structures
  29. Aeroelastic Shape Optimization of a Flapping Wing
  30. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects
  31. Evaluation of Quasi-Static Gust Loads Certification Methods for High-Altitude Long-Endurance Aircraft
  32. Continuum Sensitivity Method for Aeroelastic Shape Design Problems
  33. Aeroelastic Optimization of Membrane Prestress on a Flapping Wing
  34. Parametric Representation and Shape Optimization of Flapping Micro Air Vehicle Wings
  35. Thrust and Efficiency Optimization of a Harmonically Deforming Thin Airfoil for MAV Design
  36. Aeroelastic Scaling of a Joined Wing for Nonlinear Geometric Stiffness
  37. Experimental Nonlinear Static Deflections of a Subscale Joined Wing
  38. Continuum Shape Sensitivity for Nonlinear Transient Aeroelastic Gust Response
  39. Design Optimization of a WR-90 Slotted Waveguide Antenna Stiffened Structures
  40. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations
  41. Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles
  42. Thrust and Efficiency Optimization of a Harmonically Deforming Thin Airfoil for MAV Design
  43. Least-Squares Continuous Sensitivity Shape Optimization for Structural Elasticity Applications
  44. Multidisciplinary Design for Flight Test of a Scaled Joined Wing SensorCraft
  45. F-16 Ventral Fin Buffet Alleviation Using Piezoelectric Actuators
  46. Fluid-Structure Transient Gust Sensitivity Using Least-Squares Continuous Sensitivity Analysis
  47. Tools for Conceptual Design and Engineering Analysis of Micro Air Vehicles
  48. Large-Scale Multidisciplinary Validation of Enriched Multipoint Cubic Approximations
  49. Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft
  50. Aeroelastic Scaling for Verification and Evaluation of Geometric Nonlinearity on a Joined-Wing Aircraft Model
  51. Advantages and Disadvantages of a Simultaneously Coupled Least-Squares Finite Element Formulation for Fluid-Structure Interaction
  52. Continuous Sensitivity Analysis of Fluid-Structure Interaction Problems Using Least-Squares Finite Elements
  53. Alleviation of buffet-induced vibration using piezoelectric actuators
  54. Aeroelastic Scaling for a Static Nonlinear Response of a Joined-Wing Aircraft
  55. Multi-Disciplinary Optimization of a Distributed Actuation System in a Flexible Morphing Wing
  56. Experimental Dynamic Response of a Munition of Various Weights Impacting a Low Pressure Airbag at Various Speeds
  57. Large Scale Optimization Using Multipoint Cubic Approximation
  58. The Least-Squares Finite Element Method Applied to Fluid-Structure Interation Problems
  59. Non-Linear Aeroelastic Scaling of a Joined-Wing Concept
  60. Structural Design of Wing Twist for Pitch Control of Joined Wing SensorCraft
  61. Joined-Wing Sensor-Craft Configuration Design
  62. Estimation of structural reliability for Gaussian random fields
  63. VIBRATION AND TRANSONIC FLUTTER ANALYSIS FOR F-16 STORES CONFIGURATION CLEARANCE
  64. Efficient Successive Reanalysis Technique for Engineering Structures
  65. Accelerated engineering design optimization using successive matrix inversion method
  66. Reliability based optimisation of engineering structures under imprecise information
  67. Robust design of mechanical systems via stochastic expansion
  68. Joined-Wing Aeroelastic Design with Geometric Nonlinearity
  69. Dynamic Response of a Munition to a Low Pressure Airbag
  70. Reliability-Based Design Optimization under Imprecise Uncertainty
  71. Sensor-Craft Structural Optimization and Analytical Certification
  72. An approximation approach for uncertainty quantification using evidence theory
  73. Optimization Process for Configuration of Flexible Joined-Wing
  74. Accelerated Engineering Design Optimization Using Successive Matrix Inversion Method
  75. Optimization of Stochastic Mechanical Systems using Polynomial Chaos Expansion
  76. Successive Matrix Inversion Method for Reanalysis of Engineering Structural Systems
  77. Comparison of evidence theory and Bayesian theory for uncertainty modeling
  78. Structural reliability under non-Gaussian stochastic behavior
  79. Epistemic uncertainty quantification techniques including evidence theory for large-scale structures
  80. Joined-Wing Sensor-Craft Configuration Design
  81. An Efficient Successive Reanalysis Technique for Engineering Structures
  82. SensorCraft Structural Optimization and Analytical Certification
  83. Structurally Integrated Antennas on a Joined-Wing Aircraft
  84. Aero-Structural Coupling and Sensitivity of a Joined-Wing SensorCraft
  85. Polynomial Chaos Expansion with Latin Hypercube Sampling for Predicting Response Variability
  86. Reliability Analysis of a Large Computational Model Using Polynomial Chaos Expansion
  87. Structural Design Optimization Based on Reliability Analysis Using Evidence Theory
  88. Propagation of non-Gaussian stochastic behavior using the polynomial chaos expansion
  89. Uncertainty quantification using evidence theory with a cost-effective algorithm
  90. Multipoint Cubic Surrogate Functions for Sequential Approximate Optimization
  91. Sensitivity Analysis of Structural Response Uncertainty Propagation Using Evidence Theory
  92. Uncertainty Quantification of Structural Response Using Evidence Theory
  93. A Joined-Wing Structural Weight Modeling Study
  94. Non-Linear Transonic Flutter Analysis for F-16 Stores Configuration Clearance
  95. Sequential multipoint quadratic approximation for numerical optimization
  96. Comment on 'Improved first-order approximation to eigenvalues and eigenvectors'
  97. Methodology for Implementing Fracture Mechanics in Global Structural Design of Aircraft
  98. Discrete-time, mixed-norm control synthesis applied to aircraft terrain following
  99. Methodology for implementing fracture mechanics in global structural design of aircraft
  100. Finite element model tuning using automated structural optimization system software
  101. A rank two Hessian matrix update for sequential quadratic approximation
  102. Multipoint quadratic approximation for numerical optimization
  103. Multi-point constraint approximation in structural optimization
  104. Effect of modal sensitivity on flutter eigenvalue derivatives
  105. Design of frames against buckling using a Rayleigh quotient approximation
  106. Integrated Structural Design and Vibration Suppression Using Independent Modal-Space Control
  107. Design of frames against buckling using a Rayleigh Quotient Approximation