All Stories

  1. Multi-Scale Microstructure-Informed Modeling of Residual Stresses and Distortions in Additive Friction Stir Deposition
  2. Optimization of a Tapered Deployable Space Structure
  3. Rapid Coupled Loads Analysis and Trade Studies Using Norton-Thevenin Receptance Coupling
  4. Tightly Coupled Geometrically Nonlinear Structural and Aeroelastic Analysis of Flexible Wing Plate Model
  5. Sensitivity Analysis of Laminated Thin Ply Laminated Carbon Composites
  6. Topology Optimization With Integrated Density and Angle Variables for Composite Structures
  7. Unsteady Metric-Based Adaptation via Koopman Expansion
  8. Implementation of Manufacturability Constraints for NASTRAN-based Design Optimization of VAT Fiber Composite Structures
  9. Design Framework for Optimization of Curvilinearly Stiffened Variable Stiffness Composite Laminates with Direct Fiber Angle Parameterization
  10. Vibroacoustic studies on structurally optimized Pareto designs of curved composite stiffened panel
  11. Multidisciplinary Design Analysis and Optimization of Space Vehicle Structures
  12. Aeroelastic Analysis and Wind Tunnel Flutter Testing of Inflatable Tethered Wing
  13. Tow Path Recovery and Quantification of Manufacturing Constraints for Tow Steered Composite Structures
  14. Novel Airplane Design Configurations using Truss-braced Wing and Nature Stiffening Members
  15. Two-level Weight Optimization of Composite Laminates using Integer Programming
  16. Structural and Aeroelastic Design, Analysis, and Experiments of Inflatable Airborne Wings
  17. High Altitude Airborne Wind Energy
  18. Development of an Artificial Intelligence System to Design of Structures using Reinforcement Learning: Proof of Concept
  19. Analysis, Design, and Experiments of Metal Flat Plate and Foam Airfoil Flutter Test Articles
  20. Distributed Design Optimization of Large Aspect Ratio Wing Aircraft with Rapid Transonic Flutter Analysis in Linux
  21. Unfurlable Space Structure Optimization
  22. Skin-Stringer Assembly Using Radial Basis Functions for Curvilinearly Stiffened Panels
  23. ALGA: Active Learning-Based Genetic Algorithm for Accelerating Structural Optimization
  24. Failure of Hexagonal and Triangular Honeycomb Core Sandwich Panels
  25. Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory
  26. Modeling, Design, and Flight Testing of Three Flutter Controllers for a Flying-Wing Drone
  27. Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization
  28. Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows
  29. Nonintrusive Computation of Rigid-Body/Flexible-Body Coupling Integrals
  30. Lowest Twelve Frequencies of Sandwich Plates Using Third-Order Shear-Normal Deformation Theory
  31. Buckling Load Maximization of Curvilinearly Stiffened Tow-Steered Laminates
  32. Actuator energy and drag minimization of a blended-wing-body with variable-camber continuous trailing-edge flaps
  33. Investigation of Controllability Gramian as Control Objective in MDAO Framework
  34. Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs
  35. Prestressed Vibration of Stiffened Variable-Angle Tow Laminated Plates
  36. Structural Optimization of Internal Structure of Aircraft Wings with Curvilinear Spars and Ribs
  37. Thermal Buckling Analysis and Optimization of Curvilinearly Stiffened Plates with Variable Angle Tow Laminates
  38. Flight-Dynamics and Flutter Analysis and Control of an MDAO-Designed Flying-Wing Research Drone
  39. Finite Element Model Updating of Composite Flying-wing Aircraft using Global/Local Optimization
  40. Self-Learning, Adaptive Software for Aerospace Engineering Applications: Example of Oblique Shocks in Supersonic Flow
  41. Effect of Centrifugal Stiffening on the Natural Frequencies of a Flexible Drone in Roll Maneuvers
  42. Structural Design and Optimization of Commercial Vehicles Chassis under Multiple Load Cases and Constraints
  43. Numerical Prediction of Interference Drag of a Strut-Surface Intersection in Supersonic Flow
  44. Failure of Alternate Honeycomb Core Sandwich Panels
  45. Crush Dynamics and Shear Failure of Alternate Sandwich Panel Honeycomb Core for Space Structures
  46. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method
  47. Hybrid Optimization of Curvilinearly Stiffened Shells Using Parallel Processing
  48. Stochastic critical stress intensity factor response of single edge notched laminated composite plate using displacement correlation method
  49. Nonstationary Random Vibration Analysis of Wing with Geometric Nonlinearity Under Correlated Excitation
  50. Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications
  51. Aeroelastic Control-Oriented Modeling of an Airbreathing Hypersonic Vehicle
  52. Global-local Aeroelastic Optimization of Internal Structure of Transport Aircraft wing
  53. Static Aeroelastic Optimization of Aircraft Wing with Multiple Surfaces
  54. State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization
  55. Optimal Design of Curvilinearly Stiffened Shells
  56. Honeycomb Core Failure Prediction in Joint using Nonlinear Finite Element Analysis
  57. Finite Element Model Updating of A Small Flexible Composite UAV
  58. Multidisciplinary Design Analysis and Optimization of Performance Adaptive Aeroelastic Wings
  59. Integrated Aircraft Parametric Structural & Outer Mold Line Geometry Modeling Software
  60. Conceptual Design of Complex Transonic Aircraft Configurations with Flutter Prediction
  61. SpaRibs Geometry Parameterization for Wings with Multiple Sections using Single Design Space
  62. Honeycomb Core Buckling Due to Transverse Compression
  63. Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads
  64. Transonic Aerodynamics Analysis for Multidisciplinary Design Optimization Applications
  65. Aeroservoelastic Optimization of Wing Structure Using Curvilinear Spars and Ribs (SpaRibs)
  66. Control Power Optimization Using Artificial Intelligence For Forward Swept Wing And Hybrid Wing Body Aircraft
  67. Accurate Computing of Higher Vibration Modes of Thin Flexible Structures
  68. Free Vibration Analysis of Integrally Stiffened Plates with Plate-Strip Stiffeners
  69. A Physics-Based Methodology for Cantilever and Strut-Braced Wing Weight Estimation
  70. Transonic Aeroelastic Analysis for Multidisciplinary Design Optimization Applications
  71. Damped Free Vibration Response of An Adhesively Bonded Stiffened Plate with Plate-Strip Stiffeners
  72. Thermo-Mechanical Analysis and Design of Threaded Fasteners
  73. Aeroelastic Control-oriented Modeling of an Air-breathing Hypersonic Vehicle
  74. Vibrational Analysis of Unitized Curvilinearly Stiffened Composite Panels Subjected to In-plane Loads
  75. Flight-Dynamics and Flutter Modeling and Analyses of a Flexible Flying-Wing Drone - Invited
  76. Non-Stationary Random Vibration Analysis Using Multi-Correlated Random Processes Excitations
  77. Effect of Flutter on the Multidisciplinary Design Optimization of Truss-Braced-Wing Aircraft
  78. Comparative Assessment of Strut-Braced and Truss-Braced Wing Configurations Using Multidisciplinary Design Optimization
  79. Experimental Validation of the EBF3PanelOpt Vibroacoustic Analysis of Stiffened Panels
  80. Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft
  81. Vibration and Buckling Analysis of Curvilinearly Stiffened Plates Using Finite Element Method
  82. Integrated Global Wing and Local Panel Optimization of Aircraft Wing
  83. Assessment of Existing Models for Honeycomb Homogenized Properties
  84. A Novel Scheme to Accurately Compute Higher Vibration Modes using the Ritz Method and a Two-point BVP Solver
  85. Free Vibration Analysis of an Integrally Stiffened Plate with Plate-Strip Stiffeners using a Set of Static Timoshenko Beam Functions
  86. Nonlinear Aeroelastic Analysis of SUGAR Truss-braced Wing (TBW) Wind-tunnel Model (WTM) Under In-plane Loads
  87. Aeroelastic Analysis and Optimization of Flexible Wing Aircraft with a Novel Control Effector
  88. A Comparison of FEM and Semi-Analytical Method in the Buckling and Vibration of Non-Prismatic Columns under Tip Force and Self-Weight
  89. Adhesively Bonded Joint Modeling Approaches using Linear Finite Element Analysis
  90. Finite Element Approach to the Static, Vibration and Buckling Analysis of Curvilinearly Stiffened Plates
  91. Free Vibration Analysis of Curvilinearly Stiffened Cylindrical Shells
  92. Parametric Geometry Model for Design Studies of Tailless Supersonic Aircraft
  93. Aircraft Conceptual Design: Tools Evaluation
  94. Fabrication and Characterization of 3-D printed Heat Flux Sensors for Advanced Wind Tunnel Models and Improved CFD Validation
  95. Multidisciplinary Design Optimization of a Truss Braced Wing Concept
  96. Buckling Analysis of Curvilinearly Stiffened Composite Panels with Cracks
  97. Multidisciplinary Design Optimization of Subsonic Strut-Braced Wing Aircraft
  98. Nonlinear Aeroelastic Analysis of a Truss Based Wing Aircraft
  99. Global/Local Multidisciplinary Design Optimization of Subsonic Wing
  100. Degradation in Cellular Core Mechanical Properties due to Transverse Compression
  101. Experimental Validation of the EBF3PanelOpt Vibro-acoustic Analysis of Panels with Straight and Curvilinear sti[|#11#|]ffeners