Problems of rocket exhaust plume interactions.
Three dimensional interaction of multirocket vehicle exhaust jet plumes calculated, using finite difference analog to inviscid flow equations
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Three dimensional interaction of multirocket vehicle exhaust jet plumes calculated, using finite difference analog to inviscid flow equations
Back flow from jet plumes in vacuum, determining particle density at surrounding points forward of jet nozzle in vacuum due to gas exhausted
Shock tube simulation of rocket exhaust plumes and effects on vehicles in space environment
Data from absorption coefficients and fine-structure parameters measured for water vapor have been incorporated in an analytic program useful in evaluating heating by radiation from the exhaust plume of a large rocket.
Engineering methods and computer programs for predicting convective heat flux and pressure in flow regimes of low density plume impingement
Computer programs and engineering methods for calculating heating rates and forces in jet plume impingement problems
Pitot pressure distributions of jets measured in order to determine plume characteristics of Saturn cluster model
Plume flow field analysis for liquid propellant rocket engines
Band model for calculating radiative heat transfer from Saturn exhaust plumes
Jet plume induced, flow separation on lifting entry model flat bottom by pressure distribution analysis
Exhaust plume characteristics for R4D engine used by CSM reaction control system
Exhaust plume characteristics for rocket engines in conjunction with orbital workshop systems
Analytical framework for viscous and chemically reacting plume
Crew radiation dose from gas-core nuclear rocket plume
Lunar module reaction control system engine exhaust plume evaluation tests in space environment simulation laboratories
Jet-plume-induced flow separation on asymmetric bodies at 3.00, 4.50, and 6.00 Mach numbers
Exhaust plume flow field of Skylab R-4D attitude control motors