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Heather P. Houlden
Observed names:
Heather Houlden,
Houlden, Heather P.
Observed institutions:
Langley Research Center,
ViGYAN (United States),
American Institute of Aeronautics and Astronautics
OpenAlex ID:
A5044930214
Development of a Wind Tunnel Active Vibration Reduction System
2007
·
Sundareswara Balakrishna
, Heather Houlden
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
·
32
Detailed Uncertainty Analysis for Ares I Ascent Aerodynamics Wind Tunnel Database
2008
·
Michael Hemsch
, Heather Houlden
, et al.
·
AIAA Aerodynamic Measurement Technology and Ground Testing Conference
·
20
PDF
Innovative Control Effectors (ICE) Phase III
1997
·
Kenneth M. Dorsett
, Scott P. Fears
, et al.
·
Defense Technical Information Center (DTIC)
·
18
Quantification of the Uncertainties for the Ares I A106 Ascent Aerodynamic Database
2010
·
Heather Houlden
, Amber Favaregh
, et al.
·
AIAA Aerodynamic Measurement Technology and Ground Testing Conference
·
16
PDF
Space Launch System Ascent Static Aerodynamics Database Development
2014
·
Jeremy T. Pinier
, David W. Bennett
, et al.
·
AIAA Aerospace Sciences Meeting
·
13
Measurement of Force Balance Repeatability and Reproducibility in the NTF
2004
·
Michael Hemsch
, David Tuttle
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
·
13
Ascent Aerodynamic Force and Moment Database Development for the Space Launch System
2019
·
Patrick R. Shea
, Jeremy T. Pinier
, et al.
·
AIAA AVIATION Forum
·
5
Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
2019
·
Courtney S. Winski
, Paul M. Danehy
, et al.
·
AIAA AVIATION Forum
·
5
PDF
Space Launch System Aerodynamic Database Uncertainty Quantification Methodologies
2016
·
Amber L. Favaregh
, Heather Houlden
, et al.
·
AIAA Aerospace Sciences Meeting
·
5
Repeatability Modeling for Wind-Tunnel Measurements: Results for Three Langley Facilities
2014
·
Michael J. Hemsch
, Heather P. Houlden
·
AIAA Aerospace Sciences Meeting
·
3
PDF
Testing of Two Mars Powered Descent Vehicle Concepts in the Langley Unitary Plan Wind Tunnel
2024
·
Karl T. Edquist
, Bryan Falman
, et al.
·
AIAA AVIATION Forum
·
2
Uncertainty Quantification for Launch Vehicle Aerodynamic Lineloads
2020
·
Thomas J. Wignall
, Heather Houlden
·
AIAA SciTech Forum
·
2
Computational Analysis of Two Mars Powered Descent Vehicle Concepts Tested in the Langley Unitary Plan Wind Tunnel
2024
·
Karl T. Edquist
, Stephen Alter
, et al.
·
AIAA AVIATION Forum
·
1
Informing the Space Launch System Booster Separation Initial CFD Run Matrix with Observed Parametric Sensitivity
2022
·
Michael W. Lee
, Aaron Burkhead
, et al.
·
AIAA SciTech Forum
·
1
Ascent Aerodynamic Force and Moment Database Development for the Space Launch System
2019
·
Patrick R. Shea
, Jeremy T. Pinier
, et al.
·
AIAA SciTech Forum
·
1
Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
2019
·
Courtney S. Winski
, Paul M. Danehy
, et al.
·
AIAA SciTech Forum
·
1
Evaluation of CFD as a Surrogate for Wind-Tunnel Testing - Experimental Uncertainty Quantification
2021
·
Erin Hubbard
, Heather Houlden
·
AIAA AVIATION Forum
Withdrawal: Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements
2019
·
Courtney S. Winski
, Paul M. Danehy
, et al.
·
AIAA SciTech Forum
Withdrawal: Ascent Aerodynamic Force and Moment Database Development for the Space Launch System
2019
·
Patrick R. Shea
, Jeremy T. Pinier
, et al.
·
AIAA SciTech Forum
Quantification of the Uncertainties for the Space Launch System Liftoff/Transition and Ascent Databases
2016
·
Amber L. Favaregh
, Heather Houlden
, et al.
·
NASA Technical Reports Server (NASA)
Development of multi-dimensional wavelet methods for simulation aerodynamic modeling
2001
·
Heather Houlden
, Ed Parlette
, et al.
·
AIAA Aerospace Sciences Meeting and Exhibit
On the application of wavelet methods to simulation aerodynamic modeling
2000
·
Heather Houlden
, Ed Parlette
, et al.
·
AIAA Aerodynamic Measurement Technology and Ground Testing Conference
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Works count:
24
Citation count:
138
H-index:
6
I10-index:
6
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