All Stories

  1. Linearized Rigid-Body Dynamics of Asymmetric Aircraft
  2. Evaluation of First-Order Actuator Dynamics and Linear Controller for a Bio-Inspired Rotating Empennage Fighter Aircraft
  3. Stick-Fixed Maneuver Points in Roll, Pitch, and Yaw and Associated Handling Qualities
  4. Aerodynamic State Determination Using Multi-Port Pitot Probes with Arbitrary Port Locations
  5. Using a Topology Optimization Results Interpreter on the Frame of an Aircraft with a Bio-Inspired Rotating Empennage
  6. Characterization of the Common Research Model Wing for Low-Fidelity Aerostructural Analysis
  7. Computational Design Methodology of Adaptive Outer Mold Line for Robust Low En-Route Noise of a Supersonic Aircraft
  8. Controlling Roll-Yaw Coupling with Aileron Placement and Wing Twist
  9. Comparison of Theoretical and High-Fidelity Aerostructural Solutions
  10. General Approach to Lifting-Line Theory, Applied to Wings with Sweep
  11. Adverse-Yaw Control During Roll for a Class of Optimal Lift Distributions
  12. Minimum Induced Drag for Tapered Wings Including Structural Constraints
  13. Analytic and computational analysis of wing twist to minimize induced drag during roll
  14. Aerodynamic Centers of Arbitrary Airfoils Below Stall
  15. Minimizing Induced Drag with Weight Distribution, Lift Distribution, Wingspan, and Wing-Structure Weight
  16. Minimum-Frequency Spanwise Twist for Yawing-Moment Control During Roll
  17. Experimental Evaluation of the Performance of Parabolic Flaps
  18. A Multi-Fidelity Prediction of Aerodynamic and Sonic Boom Characteristics of the JAXA Wing Body
  19. Comparison of Induced and Parasitic Drag on Wings with Minimum Induced Drag
  20. Effect of Sweep on Airfoil Section Properties
  21. Procedure for the Calculation of the Perceived Loudness of Sonic Booms
  22. A Methodology for Roll Control of Morphing Aircraft
  23. Lifting-Line Analysis of Wing Twist to Minimize Induced Drag During Pure Rolling Motion
  24. Prediction of Sonic Boom Loudness Using High-Order Panel Methods for the Near-Field Solution
  25. Extended 3D Class/Shape Transformation equations for multicomponent aircraft assemblies
  26. Aerodynamic Center at the Root of Swept, Elliptic Wings in Inviscid Flow
  27. Designing Wing Twist or Planform Distributions for Specified Lift Distributions
  28. Minimizing Induced Drag with Lift Distribution and Wingspan
  29. Geometry and Aerodynamic Performance of Parabolic Trailing-Edge Flaps
  30. Aerodynamic Centers of Arbitrary Airfoils
  31. Experimental Results for a Variable Camber Compliant Wing
  32. Aerodynamic Shape Optimization of Morphing Wings at Multiple Flight Conditions
  33. Designing Wings with Fixed Twist for Minimum Induced Drag
  34. Validation of Flux Correction on Three-Dimensional Strand Grids with an Overset Cartesian Grid
  35. Wing Optimization using Dual Number Automatic Differentiation in MachUp
  36. Propulsion Theory of Flapping Airfoils: Comparison with Computational Fluid Dynamics
  37. Propulsion Theory of Flapping Airfoils, Comparison with Computational Fluid Dynamics
  38. Momentum Theory with Slipstream Rotation Applied to Wind Turbines
  39. Lifting-Line Predictions for Induced Drag and Lift in Ground Effect
  40. Decomposed Lifting-Line Predictions and Optimization for Propulsive Efficiency of Flapping Wings
  41. Application of an Energy-Vorticity Turbulence Model to Fully Rough Pipe Flow
  42. Smooth-Wall Boundary Conditions for Dissipation-Based Turbulence Models
  43. Pitch Dynamics of Unmanned Aerial Vehicles
  44. A Numerical Blade Element Approach to Estimating Propeller Flowfields
  45. Optimization of Iris, a Small Autonomous Surveillance UAV
  46. A Lifting-Line Approach to Estimating Propeller/Wing Interactions