Add to ORKGOperating characteristics of the Langley Mach 7 Scramjet Test Facility are described. The facility is designed for testing airframe integrated scramjet (supersonic combustion ramjet) engine models. Features include duplication of the flight Mach number total enthalpy, flight altitude simulation, and simulation of engine airframe integration effects such a bow shock wave precompression and boundary layer ingestion by the engine. Data obtained from facility calibration and from tests of a hydrogen burning, airframe integrated scramjet are discussed. An adverse interaction between the facility flow and the scramjet engine flow during combustion of the fuel is described
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Tests of the Hyper-X scramjet engine flowpath have been conducted in the HYPULSE shock tunnel at con...
Reports by the staff of the University of Oueensland on various research studies related to the adva...
An experimental research program conducted to expand the operational capabilities of the NASA Langle...
An engine test facility was constructed at the NASA Langley Research Center in support of a superson...
A summary of the research activities is presented along with the design and analysis of an integrate...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Research programs at the NASA Langley Research Center on the development of airframe-integrated scra...
The results of a preliminary investigation of the combustion of hydrogen fuel at hypersonic flow con...
A study of the suitabiiity of ground-based faciiities for simulating the iiow and combustion in scra...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Results are presented of an experiment to investigate the behavior at Mach 4 flight conditions of th...
While typically analysed through ground-based impulse facilities, scramjets experience significant h...
Tests were conducted to determine the performance of a hydrogen burner used to produce a test gas th...
The aerodynamic drag and fuel distribution patterns of injectors designed for a supersonic combustio...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Tests of the Hyper-X scramjet engine flowpath have been conducted in the HYPULSE shock tunnel at con...
Reports by the staff of the University of Oueensland on various research studies related to the adva...
An experimental research program conducted to expand the operational capabilities of the NASA Langle...
An engine test facility was constructed at the NASA Langley Research Center in support of a superson...
A summary of the research activities is presented along with the design and analysis of an integrate...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Research programs at the NASA Langley Research Center on the development of airframe-integrated scra...
The results of a preliminary investigation of the combustion of hydrogen fuel at hypersonic flow con...
A study of the suitabiiity of ground-based faciiities for simulating the iiow and combustion in scra...
Reports by the staff of the University of Queensland on various research studies related to the adva...
Results are presented of an experiment to investigate the behavior at Mach 4 flight conditions of th...
While typically analysed through ground-based impulse facilities, scramjets experience significant h...
Tests were conducted to determine the performance of a hydrogen burner used to produce a test gas th...
The aerodynamic drag and fuel distribution patterns of injectors designed for a supersonic combustio...
The NASA Langley Research Center has conducted hypersonic propulsion research since the 1960s. A var...
Tests of the Hyper-X scramjet engine flowpath have been conducted in the HYPULSE shock tunnel at con...
Reports by the staff of the University of Oueensland on various research studies related to the adva...