All Stories

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