Uncertainty Analysis of Mars Entry Flows over a Hypersonic Inflatable Aerodynamic Decelerator-Reference-Cited by-同舟云学术

Uncertainty Analysis of Mars Entry Flows over a Hypersonic Inflatable Aerodynamic Decelerator

Published:2015-05 Issue:3 Volume:52 Page:776-788
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Brune Andrew J.¹,West Thomas K.¹,Hosder Serhat¹,Edquist Karl T.²

Affiliation:

1. Department of Aerospace and Mechanical Engineering, Missouri University of Science and Technology, Rolla, Missouri 65409

2. Atmospheric Flight and Entry Systems Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33131

Reference29 articles.

1. Overview of the NASA Entry, Descent and Landing Systems Analysis Stud

2. Dwyer-CiancoloA. M.DavisJ. L.EngelundW. C.KomarD. R.QueenE. M.SamarehJ. A.WayD. W.ZangT. A. “Entry, Descent, and Landing Systems Analysis Study: Phase 2 Report on Exploration Feed-Forward Systems,” NASA TR-TM-217055, Feb. 2011.

3. Uncertainty and Sensitivity Analysis for Reentry Flows with Inherent and Model-Form Uncertainties

4. Efficient Uncertainty Quantification in Multidisciplinary Analysis of a Reusable Launch Vehicle

5. Efficient Sampling for Non-Intrusive Polynomial Chaos Applications with Multiple Uncertain Input Variables

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