An analysis of the coupled chemically reacting boundary layer and charring ablator, part 1 Summary report
Analyses and finite difference procedure for predicting transient in-depth response of charring ablation materials
Bartlett, E. P.↗
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An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 3 - Nonsimilar solution of the multicomponent laminar boundary layer by an integral matrix method
Laminar boundary layer problems solved by integral matrix methods
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 2 - Finite difference solution for the in-depth response of charring materials considering surface chemical and energy balances
Computer program for finite difference equation analysis of in-depth response of materials exposed to high temperature environment
Moyer, C. B.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 4 - A unified approximation for mixture transport properties for multicomponent boundary-layer applications
Bifurcation approximation for binary and thermal diffusion coefficients, mixture viscosity, and thermal conductivity of laminar boundary layer
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 5 - A general approach to the thermochemical solution of mixed equilibrium-nonequilibrium, homogeneous or heterogeneous systems
Computer program for solutions to equilibrium and nonequilibrium chemical state relations for open and closed thermodynamic systems
Kendall, R. M.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 6 - An approach for characterizing charring ablator response with in-depth coking reactions
Coking reactions of pyrolysis gas in charring ablation material
Rindal, R. A.↗
Producing holograms of reacting sprays in liquid propellant rocket engines, phase 2 Interim report, 3 Apr. - 2 May 1968
Pulsed ruby laser holograms of hypergolic rocket propellants combustion processes
Matthews, B. J.↗
One-dimensional two-phase reacting-gas nonequilibrium performance program. volume 2 - program listings and flow charts
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Axisymmetric reacting gas nonequilibrium performance program. volume 1 - engineering and programming description
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One-dimensional reacting gas nonequilibrium performance program. volume 1 - engineering and programming description
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One-dimensional reacting gas nonequilibrium performance program. volume 2 - program listings and flow charts
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Axisymmetric reacting gas nonequilibrium performance program. volume 2 - program listings and flow charts
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Further studies of the coupled chemically reacting boundary layer and charring ablator. Part 3 - A nongrey radiation transport model suitable for use in ablation-product contaminated boundary layers
Nongray radiation transport model for use in ablator-contaminated boundary layers
Nicolet, W. E.↗
Further studies of the coupled chemically reacting boundary layer and charring ablator. Part 4 - Nonsimilar solution of an incompressible turbulent boundary layer by an integral matrix method
Nonsimilar solution of incompressible turbulent boundary layer by integral matrix method
Anderson, L. W.↗
A solution of the inviscid-viscid equations with applications to bounded and unbounded multicomponent reacting flows.
Viscid-inviscid equations solution, describing flows with coupled mixing, combustion and lateral pressure gradients
Edelman, R. B.↗
Microthrusters employing catalytically reacted N2-O2-H2 gas mixtures, Tridyne
Spacecraft attitude control microthrustors utilizing catalytically reactive gas mixtures during pulse mode and steady state operation
Barber, H. E.↗
Modeling reacting gas flow in the char layer of an ablator
Nonequilibrium modeling of pyrolysis gas products flow through char layer of ablative heat shield
April, G. C.↗
Solutions for Reacting and Nonreacting Viscous Shock Layers with Multicomponent Diffusion and Mass Injection
Numerical solutions are presented for the viscous shocklayer equations where the chemistry is treated as being either frozen, equilibrium, or nonequilibrium. Also the effects of the diffusion model, surface catalyticity, and mass injection on surface transport and flow parameters are considered. The equilibrium calculations for air species using multicomponent: diffusion provide solutions previously unavailable. The viscous shock-layer equations are solved by using an implicit finite-difference scheme. The flow is treated as a mixture of inert and thermally perfect species. Also the flow is assumed to be in vibrational equilibrium. All calculations are for a 45 deg hyperboloid. The flight conditions are those for various altitudes and velocities in the earth's atmosphere. Data are presented showing the effects of the chemical models; diffusion models; surface catalyticity; and mass injection of air, water, and ablation products on heat transfer; skin friction; shock stand-off distance; wall pressure distribution; and tangential velocity, temperature, and species profiles.
Moss, J. N.↗