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Experimental study of the thermal erosion in a subscale solid-propellant launcher
Yeu Pin Yeh
, Kenneth K. Kuo
,
F. Bill Cheung
, Thomas A. Litzinger
Mechanical Engineering
Leonhard Center for the Enhancement of Engineering Education
Materials Research Institute (MRI)
Research output
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Contribution to conference
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peer-review
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Dive into the research topics of 'Experimental study of the thermal erosion in a subscale solid-propellant launcher'. Together they form a unique fingerprint.
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Keyphrases
Nozzle
100%
Solid Propellant
100%
Launcher
100%
Thermal Erosion
100%
Transient Pressure
75%
Rocket Motor
75%
Ablative Materials
75%
Efflux
50%
Material Erosion
50%
Lumped Parameter Model
25%
Pressure Response
25%
Insulation
25%
Nozzle Configuration
25%
Erosion Depth
25%
Flat Surface
25%
Two-hole
25%
Fourth-order Runge-Kutta Method
25%
Surface Contour
25%
Plenum Chamber
25%
Depth Contours
25%
Eroded Area
25%
Throat Area
25%
Engineering
Transients
100%
Rocket Engine
100%
Pressure Response
100%
Material Erosion
66%
Lumped Parameter
33%
Fourth Order
33%
Kutta Method
33%
Plenum Chamber
33%
Flat Surface
33%
Throat Area
33%
Earth and Planetary Sciences
Experimental Study
100%
Transient Pressure
100%
Solid Propellant
100%
Rocket Engine
100%
Flat Surface
33%
Material Science
Ablative Material
100%
Solid Propellant
100%
Surface (Surface Science)
66%