All Stories

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