Two and three-dimensional boundary layer analysis for highly cooled bodies.
Turbulent two and three dimensional boundary layer growth and characteristics of reentry vehicle
Myers, E. T.↗
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Results for “Reentry”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Exploratory investigations of the effects of gas injection through a porous model on separation, transition, static stability and control effectiveness of a blunt re-entry body at Mach number 7.3.
Nitrogen injection on blunt reentry body, investigating influence on separation, transition, static stability and control effectiveness
Donohoe, J. C.↗
A parametric analysis of three vehicle shapes for use as hyperbolic entry.
Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
Anderson, J. L.↗
An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle.
Operating and aerodynamic characteristics of rotor in autorotative flight analyzed for reentry from orbit
Levin, A. D.↗
Propulsive-lift landing aid for entry vehicles.
Manned reentry vehicles soft landing aid by lift engines incorporated in design, discussing performance advantages
Coward, K. S.↗
Effects of the plasma sheath on antenna performance.
Antenna radiation patterns and near field effects by solving aperture and plasma sheath problems independently in reentry communications
Hodara, H.↗
Effects of non-grey self-absorption and energy loss for blunt body flows.
Nongray self absorption and energy loss effects for blunt body flows during superorbital reentry, considering flow field and wall heat fluxes
Chin, J. H.↗
A neighboring optimum feedback control scheme based on estimated time-to-go with application to re-entry flight paths.
Neighboring optimum feedback control scheme based on estimated time-to-go applied to reentry flight paths
Bryson, A. E., Jr.↗
Propulsive-lift landing of manned entry vehicles.
Manned reentry vehicles soft landing aid by lift engines incorporated in design, discussing performance advantages
Coward, K. S.↗
Simulation of the Apollo Command Module aerodynamics at re-entry altitudes.
Apollo Command Module aerodynamics at reentry altitudes simulated by models in hypersonic flow
Boylan, D. E.↗
Convective and radiative heat transfer to an ablating body.
Convective and radiative heat transfer to reentry vehicles protected by ablation heat shields
Hoshizaki, H.↗
Biosatellite II experiment environment.
Automated laboratory in Biosatellite 2 reentry vehicle, discussing experiments
Look, B. C.↗
Radioisotope thermoelectric generator design for Voyager Surface Lander.
Radioisotope thermoelectric generator concepts for Voyager Surface Lander, noting PbTe and GeSi thermoelectrics, reentry body shapes and integration considerations
Brittain, W. M.↗
Reynolds and Mach number simulation of Apollo and Gemini re-entry and comparison with flight
Reynolds and Mach numbers simulation of Apollo and Gemini reentry compared with flight data
Griffith, B. J.↗
Study of equilibrium air total radiation Final report
High temperature air radiance over range of equilibrium gas properties for application to super orbital reentry vehicles
Source record↗
A flight measurement of optical radiation from shock-heated air by using a Trailblazer 2 vehicle
Flight measurement of optical radiation from shock heated air with Trailblazer 2 reentry vehicle
Burcher, E. E.↗
Applied mechanics
Computerized simulation of Venus atmospheric entry by earth reentry, and test program on soil response to landing loads
Source record↗
Proceedings of the Conference on the Role of Simulation in Space Technology, part B
Simulation studies and facilities for atmospheric reentry at hypersonic speeds
Source record↗