Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Mark E. Ewing"'
Autor:
Mark E. Ewing, Daron A. Isaac, H. Heath Dewey, Cory W. Smith, Zachary D. Harman, David T. Walker
Publikováno v:
Journal of Thermophysics and Heat Transfer. 37:104-118
This paper describes multidimensional modeling of ablation heat transfer with a focus on ablative insulation materials used in rocket motor nozzles. Phenomenology is discussed, and detailed three-dimensional math models are presented along with a fin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::baa3775c7e301ab5acc7ae573873e6b0
https://doi.org/10.2514/1.t6582
https://doi.org/10.2514/1.t6582
Publikováno v:
Journal of Thermophysics and Heat Transfer. 36:627-636
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5efdf4ec6b89ca8c07c3c033ffb7015
https://doi.org/10.2514/1.t6346
https://doi.org/10.2514/1.t6346
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8dc2f97da5df04baed1c2bbf6582353a
https://doi.org/10.2514/6.2023-2023
https://doi.org/10.2514/6.2023-2023
Autor:
Daron A. Isaac, Mark E. Ewing
Publikováno v:
Journal of Thermophysics and Heat Transfer. 32:118-128
Modeling of chemical equilibrium is fundamental to the analysis of rocket motors. Related modeling supports performance calculations, combustion gas properties, and important interactions between r...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f16333899627924df8dc559eef1fce83
https://doi.org/10.2514/1.t5144
https://doi.org/10.2514/1.t5144
Autor:
Mark E. Ewing, Daron A. Isaac
Publikováno v:
Journal of Thermophysics and Heat Transfer. 31:473-477
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02ebabb5abf6007a54e133b49d01119e
https://doi.org/10.2514/1.t4983
https://doi.org/10.2514/1.t4983
Autor:
Mark E. Ewing, Brian Pincock
Publikováno v:
Heat Transfer Engineering. 38:1189-1197
An isoconversional modeling approach has been considered in the modeling of heat transfer and pyrolysis in a charring material. The isoconversional approach is appealing due to the use of o...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fabb72a7163467b3cd257025b248a177
https://doi.org/10.1080/01457632.2016.1239939
https://doi.org/10.1080/01457632.2016.1239939
Publikováno v:
Journal of Verification, Validation and Uncertainty Quantification. 3
Uncertainty quantification (UQ) is gaining in maturity and importance in engineering analysis. While historical engineering analysis and design methods have relied heavily on safety factors (SF) with built-in conservatism, modern approaches require d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ea59fb8204839b0ea87d895513c0d3f
https://doi.org/10.1115/1.4041490
https://doi.org/10.1115/1.4041490
Autor:
Daron A. Isaac, Mark E. Ewing
Publikováno v:
Journal of Thermophysics and Heat Transfer. 29:551-562
Prediction of chemical equilibrium conditions is fundamental to modeling in many aerospace applications including rocket performance and ablation heat transfer. Although legacy equilibrium approaches have been in place for some time, improved methodo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47120b47d4c8b452ad0c4c1e9bf4c0d3
https://doi.org/10.2514/1.t4397
https://doi.org/10.2514/1.t4397
Publikováno v:
Journal of Thermophysics and Heat Transfer. 27:615-632
A unique numerical method has been developed for solving one-dimensional ablation heat transfer problems. This paper provides a comprehensive description of the method, along with detailed derivations of the governing equations. This methodology supp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::087e97ab3c72ed0d0fc60bbd9afb70d1
https://doi.org/10.2514/1.t4164
https://doi.org/10.2514/1.t4164
Autor:
Scott Hyde, Mark E. Ewing, Scott McHenry, Ben Goldberg, Brian D. Allen, Timothy Sojourner, Derek R. DeVries, David E. Richardson
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Reliability of solid rocket motors has steadily increased since the beginning of solid propulsion systems. Increased reliability of solid rocket motors has produced a 100 percent success rate in orbital space launched rocket systems in the United Sta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b3d84b1cd85ae53180f14a3adb72578
https://doi.org/10.2514/6.2015-3873
https://doi.org/10.2514/6.2015-3873