Single Expansion Ramp Nozzle (SERN) with large expansion ratio is normally adopted for the hypersonic aircraft in consideration of integrated aircraft / propulsion system / nozzle design. Under low Mach number and low Nozzle Pressure Ratio (NPR, the ratio of inlet total pressure to outlet static pressure) conditions, the flow in the SERN is a state of severe over-expansion, the internal resistance increased obviously, the flow quality and performance of the SERN sharply deteriorated. How to effectively improve the SERN performance under over-expanded condition has become an important issue in the integrated design of hypersonic propulsion system. The passive cavity flow control technique was introduced on the upper expansion ramp of the SER...
An experimental investigation was conducted in the NASA Lewis 10 x 10 ft supersonic Wind Tunnel to d...
The transonic performance of a dual-throat, single-expansion-ramp nozzle (SERN) was investigated wit...
Flow separation in overexpanded single expansion ramp nozzles (SERN) involves complex phenomena, suc...
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...
The present work deals with the computational study of the single expansion ramp nozzle (SERN) flows...
In order to overcome the drag at hypersonic speed, hypersonic flight vehicles require a high level o...
This paper aims to contribute to developing a potential combined cycle air-breathing engine integrat...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of v...
Abstract-- The project deals with the experimental study of Single Expansion Ramp Nozzle (SERN) flow...
Experiments have been carried out to investigate the effect of cowl length variation on performance ...
The effects of five geometric design parameters on the internal performance of single-expansion-ramp...
An investigation has been conducted at static conditions (wind off) in the static-test facility of t...
The effects of geometric design parameters on the internal performance of nonaxisymmetric single exp...
Flow separation and transitions of separation patterns are common phenomena of nozzles working with ...
An experimental investigation was conducted in the NASA Lewis 10 x 10 ft supersonic Wind Tunnel to d...
The transonic performance of a dual-throat, single-expansion-ramp nozzle (SERN) was investigated wit...
Flow separation in overexpanded single expansion ramp nozzles (SERN) involves complex phenomena, suc...
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...
The present work deals with the computational study of the single expansion ramp nozzle (SERN) flows...
In order to overcome the drag at hypersonic speed, hypersonic flight vehicles require a high level o...
This paper aims to contribute to developing a potential combined cycle air-breathing engine integrat...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of v...
Abstract-- The project deals with the experimental study of Single Expansion Ramp Nozzle (SERN) flow...
Experiments have been carried out to investigate the effect of cowl length variation on performance ...
The effects of five geometric design parameters on the internal performance of single-expansion-ramp...
An investigation has been conducted at static conditions (wind off) in the static-test facility of t...
The effects of geometric design parameters on the internal performance of nonaxisymmetric single exp...
Flow separation and transitions of separation patterns are common phenomena of nozzles working with ...
An experimental investigation was conducted in the NASA Lewis 10 x 10 ft supersonic Wind Tunnel to d...
The transonic performance of a dual-throat, single-expansion-ramp nozzle (SERN) was investigated wit...
Flow separation in overexpanded single expansion ramp nozzles (SERN) involves complex phenomena, suc...