All Stories

  1. Evaluation of Artemis I Aerodynamic Force and Moment Reconstructions and Preflight Predictions for Ascent Flight
  2. Ground Winds Experienced by the Space Launch System Rocket on the Pad before the Artemis I Launch
  3. Asymmetric Flow State Switching in the Space Launch System Block 2 Liftoff Environment
  4. Unsteady Surface Pressures on the Space Launch System Liftoff Configuration
  5. Pressure Scanners for Unsteady Pressure Measurements in Wind Tunnel Applications
  6. Experimental Identification of Bistable Flow States on the Space Launch System at Liftoff Conditions
  7. Advances in the Characterization of NASA’s Space Launch System Aerodynamic Environments
  8. Ascent Aerodynamic Force and Moment Database Development for the Space Launch System
  9. Ascent Aerodynamic Force and Moment Database Development for the Space Launch System
  10. Advances in the Characterization of NASA's Space Launch System Aerodynamic Environments
  11. Uncertainty quantification for launch vehicle databases
  12. Space Launch System Booster Separation Aerodynamic Testing at the NASA Langley Unitary Plan Wind Tunnel
  13. Space Launch System
  14. Space Launch System Liftoff and Transition Aerodynamic Characterization in the NASA Langley 14x22' Subsonic Wind Tunnel
  15. Reduced-order Model for NASA Space Launch System Liftoff Aerodynamics
  16. Sonic Boom Pressure Signature Uncertainty Calculation and Propagation to Ground Noise (Invited)
  17. Space Launch System Ascent Static Aerodynamics Database Development
  18. Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
  19. Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
  20. New Aerodynamic Data Dispersion Method with Application to Launch Vehicle Design
  21. Ares I and Ares I-X Stage Separation Aerodynamic Testing
  22. Ares I and Ares I-X Stage Separation Aerodynamic Testing
  23. New Aerodynamic Data Dispersion Method with Application to Launch Vehicle Design
  24. Aerodynamic Analyses and Database Development for Ares I Vehicle First-Stage Separation
  25. Aerodynamic Analyses and Database Development for Ares I Vehicle First-Stage Separation
  26. Asymmetric Uncertainty Expression for High Gradient Aerodynamics
  27. Constellation Program Lessons Learned in the Quantification and Use of Aerodynamic Uncertainty (Invited)
  28. A New Aerodynamic Data Dispersion Method for Launch Vehicle Design (Invited)
  29. Overview of Experimental Investigations for Ares I Launch Vehicle Development
  30. Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
  31. Ares I and Ares I-X Stage Separation Aerodynamic Testing
  32. An Empirical Reduced Order Model of the Mach 0.6 Turbulent Axisymmetric Jet
  33. Aerodynamic Analyses and Database Development for Ares I Vehicle First Stage Separation
  34. Cross-Spectral Analysis of the Pressure in a Mach 0.85 Turbulent Jet
  35. Flow Control Over a Cylindrical Turret Using Synthetic Jets
  36. Low-Dimensional Tools for Closed-Loop Flow-Control in High Reynolds Number Turbulent Flows
  37. Estimation Techniques in a Turbulent Flow Field
  38. Dual-Time PIV Investigation of the Sound Producing Region of the High-Speed Jet
  39. A Spatio-Temporal Decomposition of the Acoustic Source in a Mach 0.85 Jet
  40. Measurement of the Acceleration Field of the High-Speed Jet Sound Producing Region
  41. Proportional Closed-Loop Feedback Control of Flow Separation
  42. Flow Separation Control Using a Convection Based POD Approach
  43. Low-Order Models of the Fluctuating Wall Pressure in an Incompressible Turbulent Impinging Jet
  44. Identifying the most energetic modes of the pressure near-field region of a Mach 0.85 axisymmetric jet
  45. Experimental Development of a Reduced Order Model for Flow Sepapration Control
  46. Interactions of Zero Net-Mass Flow Actuators the Flow over NACA 4412 Foils
  47. Two-Point Correlations of the Near and Far-Field Pressure in a Transonic Jet
  48. Controller Development for Closed-Loop Feedback Control of Flows
  49. Towards Closed-Loop Feedback Control of the Flow over NACA-4412 Airfoil
  50. Feedback Control of Separated Flows
  51. Estimation techniques in a turbulent flow field
  52. Dual-Time PIV Investigation of the Sound Producing region of the Controlled and Uncontrolled High-Speed Jet