All Stories

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