Applications of a tube wind tunnel in supersonic testing.
Short duration tube wind tunnel supersonic testing, noting Saturn S-1C base heating and solid propellant rocket base burning tests
Hendershot, K. C.↗
Engineering topics
Wilson, H. B., Jr.
Publications and source records attributed to Wilson, H. B., Jr..
Results from short-duration altitude-chamber techniques for simulating rocket base heating problems.
Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
SOLID PROPELLANT ROCKET ENGINE↗
A new approach for evaluating the performance and base environment characteristics of nonconventional rocket propulsion systems.
Nonconventional rocket propulsion systems performance and base environment characteristics evaluated, using separate cold flow and combustion models
PROPULSION SYSTEM PERFORMANCE↗
A new technique for simulating rocket engine flow for study of base heating problems.
Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
LAMINAR BOUNDARY LAYER↗
A short-duration technique for simulated rocket exhaust and wind tunnel flow and its application to the study of scale effect of recirculating flow fields.
Short duration simulation of rocket exhaust products, flow duration through nozzle and effect on recirculation flow fields
FLOW FIELD↗