Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Eric C. Stern"'
Publikováno v:
Journal of Spacecraft and Rockets. 59:1475-1485
Publikováno v:
AIAA Journal. 60:2028-2038
Publikováno v:
Journal of Thermophysics and Heat Transfer. 35:288-295
Woven thermal protection systems (TPSs) are being developed for extreme heating conditions experienced during hypersonic atmospheric entry. A linear elasticity solver is used to model this new clas...
Autor:
Joseph M. Brock, Eric C. Stern, Patrick Seltner, Michael J. Aftosmis, Sebastian Willems, Ali Gülhan
Abstract The influence of the flight attitude on aerodynamic coefficients and static stability of cylindrical bodies in hypersonic flows is of interest in understanding the re/entry of space debris, meteoroid fragments, launch-vehicle stages and othe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::297c6138e02d3281db406eea8824cf26
https://doi.org/10.1007/s00348-021-03269-6
https://doi.org/10.1007/s00348-021-03269-6
Autor:
Eric C. Stern, Christopher O. Johnston
Publikováno v:
Icarus. 327:48-59
This paper develops a model for simulating the radiative flux reaching the ground originating from a meteor shock-layer and wake. The area of radiant burn measured for the Tunguska event provides a test case for the developed model. This model applie
Publikováno v:
Journal of Spacecraft and Rockets. 56:865-874
A thermal ablation model for glassy materials is proposed. The model includes mass losses from evaporation and condensation as well as from the moving molten layer driven by surface shear force and...
Publikováno v:
Journal of Spacecraft and Rockets. 56:526-535
The free-flight behavior of entry vehicles can greatly impact vehicle and mission design. Current methodologies rely heavily on ground and flight experiments, while computational fluid dynamics is ...
Autor:
Eric C. Stern, Graham V. Candler, Ioannis Nompelis, Thomas E. Schwartzentruber, Savio J. Poovathingal
Publikováno v:
Journal of Computational Physics. 380:408-426
Numerical methods are developed to simulate high temperature gas flow and coupled surface reactions, relevant to porous thermal protection systems used by hypersonic vehicles. Due to the non-continuum nature of these flows, the direct simulation Mont
Autor:
Ioannis Nompelis, Savio J. Poovathingal, Graham V. Candler, Eric C. Stern, Thomas E. Schwartzentruber
Publikováno v:
Journal of Computational Physics. 380:427-441
Micro scale simulations are performed of flow through porous (pyrolyzing) thermal protection system (TPS) materials using the direct simulation Monte Carlo (DSMC) method. DSMC results for permeability are validated with computational fluid dynamics (
Publikováno v:
AIAA Scitech 2021 Forum.