Hexcomb-Pattern Roughness Effects on Blunt-Body Transition and Heating-Reference-Cited by-同舟云学术

Hexcomb-Pattern Roughness Effects on Blunt-Body Transition and Heating

Published:2021-11 Issue:6 Volume:58 Page:1612-1635
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Hollis Brian R.¹

Affiliation:

1. NASA Langley Research Center, Hampton, VA 23681

Funder

NASA Entry Systems Modeling Project

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.A34791

Reference15 articles.

1. HollisB. R. “Experimental Investigation of Hexcomb-Pattern Roughness Effects on Transition Onset and Turbulent Heating Augmentation at Mach 6,” NASA TM-2019-220424, Nov. 2019.

2. Results & Analysis of Large Scale Article Testing in the Ames 60 MW Interaction Heating Arc Jet Facility

3. BergerK.RuferS.HollingsworthK.WrightS. “NASA Langley Aerothermodynamic Laboratory: Hypersonic Testing Capabilities,” AIAA Paper 2015-1337, Jan. 2015. 10.2514/6.2015-1337

4. HollisB. R.BergerK. T.BerryS. A.BrauckmannG. J.BuckG. M.DiFulvioM.HorvathT. J.LiechtyD. S.MerskiN. R.MurphyK. J.RuferS. J. “Entry, Descent, and Landing Aerothermodynamics: NASA Langley Experimental Capabilities and Contributions,” AIAA Paper 2014-1154, Jan. 2014. 10.2514/6.2014-1154

5. Blunt-Body Entry Vehicle Aerotherodynamics: Transition and Turbulent Heating

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1. Mars Sample Return Earth Entry System Woven Roughness Mach 6 Aeroheating Test;AIAA SCITECH 2024 Forum;2024-01-04

2. Distributed Sand-Grain Roughness Effects on Blunt Body Hypersonic Transition and Heating;AIAA SCITECH 2024 Forum;2024-01-04

3. Numerical Simulation of Boundary Layer Transition on Mach 6 Cylinder with Randomly Phased Sinusoidal Roughness;AIAA SCITECH 2024 Forum;2024-01-04

4. New Developments in NASA's Entry Systems Modeling Project;AIAA SCITECH 2023 Forum;2023-01-19

5. Correction: Hexcomb-Pattern Roughness Effects on Blunt-Body Transition and Heating;Journal of Spacecraft and Rockets;2022-03