Add to ORKGEnergy transfer in reacting flow of pyrolysis products through char layer of nylon-phenolic resin charring ablato
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
The decomposition of ablative composites is described along with the transport phenomena of pyrolysi...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Analysis of reacting flow of pyrolysis products through char layer of low density, nylon phenolic re...
Analytical model for predicting transient one- dimensional thermal performance of charring- ablator ...
The purpose of this thesis is to conduct an analytical analysis of a char-forming ablation material....
Equations for the transfer of heat through thermal protection shields are derived in finite differen...
Interaction between material ablation products and simulated atmosphere entry heat studied in tests ...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
The decomposition of ablative composites is described along with the transport phenomena of pyrolysi...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Analysis of reacting flow of pyrolysis products through char layer of low density, nylon phenolic re...
Analytical model for predicting transient one- dimensional thermal performance of charring- ablator ...
The purpose of this thesis is to conduct an analytical analysis of a char-forming ablation material....
Equations for the transfer of heat through thermal protection shields are derived in finite differen...
Interaction between material ablation products and simulated atmosphere entry heat studied in tests ...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...