A tube wind-tunnel technique for rocket propulsion 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
Sheeran, W. J.
Publications and source records attributed to Sheeran, W. J..
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.↗
A perforated-wall nozzle for variable Mach number testing.
Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
Hendershot, K. C.↗
A new concept of a variable-Mach-number perforated wall nozzle for providing a supersonic external stream in rocket-propulsion testing.
Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
Hendershot, K. G.↗
Noise from impinging, two-dimensional, underexpanded jet flows.
Noise-emission characteristics of impinging jets with two-dimensional converging-jet nozzle arrangement
CONVERGENT NOZZLE↗