All Stories

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