Add to ORKGVehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
Ablation-type thermal protection of objects traversing an atmosphere - earth and mar
Ability of several ablating materials to reduce surface heat transfer in electric arc heated airstre...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Computer program development for charring ablative materials, chemically reacting laminar boundary l...
Generalized method, including computer program, to solve problem of heat transfer and material respo...
The main objective of the present work is to demonstrate a method for prediction of aerothermal envi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Blasius boundary layer equation solution for vaporization and combustion on flat wall behind normal ...
Attached and separated boundary layers on highly cooled, ablating and nonablating models at Mach 13.
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
Ablation-type thermal protection of objects traversing an atmosphere - earth and mar
Ability of several ablating materials to reduce surface heat transfer in electric arc heated airstre...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Computer program development for charring ablative materials, chemically reacting laminar boundary l...
Generalized method, including computer program, to solve problem of heat transfer and material respo...
The main objective of the present work is to demonstrate a method for prediction of aerothermal envi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Blasius boundary layer equation solution for vaporization and combustion on flat wall behind normal ...
Attached and separated boundary layers on highly cooled, ablating and nonablating models at Mach 13.
Vehicles entering planetary atmospheres at high speed require an ablative heat shield in order to wi...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...