Add to ORKGThe effects of geometric design parameters on the internal performance of nonaxisymmetric single expansion-ramp nozzles were investigated at nozzle pressure ratios up to approximately 10. Forward-flight (cruise), vectored-thrust, and reversed-thrust nozzle operating modes were investigated
An investigation was conducted in the Langley 16-Foot Transonic Tunnel at static conditions to measu...
An investigation was conducted in the static test facility of the Langley 16-foot transonic tunnel t...
An investigation has been conducted at wind-off conditions in the stati-test facility of the Langley...
An investigation has been conducted at static conditions (wind off) in the static-test facility of t...
An investigation was conducted at wind-off conditions in the static-test facility of the Langley 16-...
The effects of five geometric design parameters on the internal performance of single-expansion-ramp...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of v...
Transonic tunnel test was performed to determine the static performance of five twin-engine nonaxisy...
The effects of geometric design parameters on two dimensional convergent-divergent nozzles were inve...
An investigation has been conducted to evaluate the effects of several geometric parameters on the i...
The Langley 16 foot transonic tunnel was used to investigate the afterbody/nozzle longitudinal aerod...
An investigation was conducted at wind-off conditions in the static-test facility of the Langley 16-...
An investigation was conducted in the static test facility of the Langley 16 Foot Transonic Tunnel i...
A translating throat single expansion-ramp nozzle (SERN) concept was designed to improve the off-des...
A translating throat single expansion-ramp nozzle (SERN) concept was designed to improve the off-des...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel at static conditions to measu...
An investigation was conducted in the static test facility of the Langley 16-foot transonic tunnel t...
An investigation has been conducted at wind-off conditions in the stati-test facility of the Langley...
An investigation has been conducted at static conditions (wind off) in the static-test facility of t...
An investigation was conducted at wind-off conditions in the static-test facility of the Langley 16-...
The effects of five geometric design parameters on the internal performance of single-expansion-ramp...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of v...
Transonic tunnel test was performed to determine the static performance of five twin-engine nonaxisy...
The effects of geometric design parameters on two dimensional convergent-divergent nozzles were inve...
An investigation has been conducted to evaluate the effects of several geometric parameters on the i...
The Langley 16 foot transonic tunnel was used to investigate the afterbody/nozzle longitudinal aerod...
An investigation was conducted at wind-off conditions in the static-test facility of the Langley 16-...
An investigation was conducted in the static test facility of the Langley 16 Foot Transonic Tunnel i...
A translating throat single expansion-ramp nozzle (SERN) concept was designed to improve the off-des...
A translating throat single expansion-ramp nozzle (SERN) concept was designed to improve the off-des...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel at static conditions to measu...
An investigation was conducted in the static test facility of the Langley 16-foot transonic tunnel t...
An investigation has been conducted at wind-off conditions in the stati-test facility of the Langley...