All Stories

  1. Testing of Two Mars Powered Descent Vehicle Concepts in the Langley Unitary Plan Wind Tunnel

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Devin Burns, Heather Houlden

  2. Computational Analysis of Two Mars Powered Descent Vehicle Concepts Tested in the Langley Unitary Plan Wind Tunnel

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Francisco Canabal, Heather Houlden

  3. Evaluation of CFD as a Surrogate for Wind-Tunnel Testing - Experimental Uncertainty Quantification

    Article • July 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden

  4. Uncertainty Quantification for Launch Vehicle Aerodynamic Lineloads

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden

  5. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Paul M Danehy, Dr Todd Lowe, Heather Houlden

  6. Ascent Aerodynamic Force and Moment Database Development for the Space Launch System

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden, Dr. Jeremy Pinier, Dr. Michael J Hemsch

  7. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Paul M Danehy, Dr Todd Lowe, Heather Houlden

  8. Ascent Aerodynamic Force and Moment Database Development for the Space Launch System

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden, Dr. Michael J Hemsch, Dr. Jeremy Pinier

  9. Uncertainty quantification for launch vehicle databases

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden, Dr. Jeremy Pinier, Dr. Michael J Hemsch

  10. Repeatability Modeling for Wind-Tunnel Measurements: Results for Three Langley Facilities

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden, Dr. Michael J Hemsch

  11. Space Launch System Ascent Static Aerodynamics Database Development

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden, Dr. Jeremy Pinier

  12. Quantification of the Uncertainties for the Ares I A106 Ascent Aerodynamic Database

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden

  13. Development of a Wind Tunnel Active Vibration Reduction System

    Article • January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden

  14. Development of multi-dimensional wavelet methods for simulation aerodynamic modeling

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden

  15. On the application of wavelet methods to simulation aerodynamic modeling

    Article • June 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Heather Houlden