Add to ORKGGeneralized method, including computer program, to solve problem of heat transfer and material response for stagnation region of blunt bodies experiencing ablatio
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Computational procedure reduces the numerical effort whenever the method of finite differences is us...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
A unique numerical method has been developed for solving one-dimensional ablation heat transfer prob...
Coupled computer code for transient thermal response and ablation of noncharring heat shields and no...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Computer program for finite difference equation analysis of in-depth response of materials exposed t...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
Ablation relationships for any type of boundary layer from transpiration cooling result
Nongray radiation transport model for use in ablator-contaminated boundary layer
Computer program development for charring ablative materials, chemically reacting laminar boundary l...
University of Minnesota Ph.D. dissertation. 2021. Major: Aerospace Engineering and Mechanics. Adviso...
Trajectory and ablation characteristics calculation for glass-tipped blunt bodies in atmospheric ent...
Ablation-type thermal protection of objects traversing an atmosphere - earth and mar
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Computational procedure reduces the numerical effort whenever the method of finite differences is us...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...
A simplified analysis is made of ablation cooling near the stagnation point of a two-dimensional or ...
A unique numerical method has been developed for solving one-dimensional ablation heat transfer prob...
Coupled computer code for transient thermal response and ablation of noncharring heat shields and no...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
Computer program for finite difference equation analysis of in-depth response of materials exposed t...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
Ablation relationships for any type of boundary layer from transpiration cooling result
Nongray radiation transport model for use in ablator-contaminated boundary layer
Computer program development for charring ablative materials, chemically reacting laminar boundary l...
University of Minnesota Ph.D. dissertation. 2021. Major: Aerospace Engineering and Mechanics. Adviso...
Trajectory and ablation characteristics calculation for glass-tipped blunt bodies in atmospheric ent...
Ablation-type thermal protection of objects traversing an atmosphere - earth and mar
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Computational procedure reduces the numerical effort whenever the method of finite differences is us...
Analyses and finite difference procedure for predicting transient in-depth response of charring abla...