All Stories

  1. Primary DOF Selection via QR Pivoting for Physical-Type Dynamic Condensation and Substructuring
  2. Dynamic Condensation for Efficient Band-Structure Calculations of 2D Periodic Structures
  3. Leading-Edge Curvature Effect on Flapping Performance of Low Aspect Ratio Wings in Forward Flight
  4. Simplifying Complex Structures: A Faster Way to Predict Vibrations
  5. Modified Iterative-Order-Reduction Substructuring Method with Interface Boundary Reduction
  6. Rigid-Foldable Polyhedral Origami
  7. Multiple-Input/Multiple-Output Random Vibration Control for Simulating a Horizontal Direction Launch Environment
  8. Publisher's Note: “Aerodynamic characteristics of flexible flapping wings depending on aspect ratio and slack angle” [Phys. Fluids 34, 051911 (2022)]
  9. Aerodynamic characteristics of flexible flapping wings depending on aspect ratio and slack angle
  10. Self-Learning MAV Under Safety-Guaranteed Flight Test Environment
  11. Automated Aerial Docking System Using Onboard Vision-Based Deep Learning
  12. Aeroelastic Behavior of Two Airfoils in Proximity
  13. New Approach to Folding a Thin-Walled Yoshimura Patterned Cylinder
  14. Performance Optimization of a Split-Type Low-Shock Separation Bolt
  15. Ground Effect on Flutter and Limit Cycle Oscillation of Airfoil with Flap
  16. Separation Behavior of Pyrotechnically Actuated Device Considering Small-Volume Effect of Combustion Chamber
  17. Interactions of the wakes of two flapping wings in hover
  18. Performance optimization of a split type low-shock separation bolt
  19. Development of Pyroshock Simulator for Shock Propagation Test
  20. Mathematical Model for the Separation Behavior of Low-Shock Separation Bolts
  21. The Trim Condition of a Hovering Insect-like Flapping-wing Micro Air Vehicle in Asymmetric Condition
  22. An efficient aerodynamic model for flapping insects
  23. Safety-Guaranteed Flight Test Environment for Micro Air Vehicles
  24. Dynamic Stability of a Hawkmoth-scale Flapping-wing Micro Air Vehicle during Forward Flight
  25. Effects of Advance Ratio on the Aerodynamic Characteristics of an Insect Wing in Forward Flight
  26. Design of Three Parameter Isolator for the RWA Disturbance Considering Flexible Structural Effects
  27. An improved quasi-steady aerodynamic model for insect wings that considers movement of the center of pressure
  28. Role of Trailing-Edge Vortices on the Hawkmothlike Flapping Wing
  29. Design of frequency-tunable mesh washer isolators using shape memory alloy actuators
  30. Longitudinal Stabilization of Hovering Flapping Wing Air Vehicles
  31. Parametric investigation on plasma streamwise vortex generators with flow around the bluff body
  32. Safety-guaranteed Flight Test Environment for Micro Air Vehicles
  33. One-equation modeling and validation of dielectric barrier discharge plasma actuator thrust
  34. Development of multi-degree-of-freedom microvibration emulator for efficient jitter test of spacecraft
  35. Experimental Study on the Unsteady Aerodynamics of a Robotic Hawkmoth Manduca sexta model
  36. Control of Wing Stroke Plane Angle for Stabilizing of a Hovering Flapping-Wing Air Vehicle