Add to ORKGDuring the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Influence of environmental conditions on thermal performance of low density charring ablato
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and arg...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Using an ablative thermal/material response code, the importance of three-dimensionality for modelin...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Ground test facility simulation of performance of charring ablators during atmospheric entr
Energy transfer in reacting flow of pyrolysis products through char layer of nylon-phenolic resin ch...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Influence of environmental conditions on thermal performance of low density charring ablato
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and arg...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Using an ablative thermal/material response code, the importance of three-dimensionality for modelin...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Ground test facility simulation of performance of charring ablators during atmospheric entr
Energy transfer in reacting flow of pyrolysis products through char layer of nylon-phenolic resin ch...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Influence of environmental conditions on thermal performance of low density charring ablato