Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected normal to supersonic airstreams.Includes bibliographical references (p. 17-18).Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected normal to supersonic airstreams.Mode of access: Internet
Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...
Turbulent mixing of compressible air in supersonic and subsonic coaxial jet flows.Includes bibliogra...
In pursuit of a more efficient and effective fuel-air mixing for a SCRAMjet combustor, this study in...
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected nor...
Prepared at Langley Research Center.N 71-34274.Includes bibliographical references (p. 14-15).Mode o...
Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...
Prepared by Fluid Mechanics and Thermal Systems, Inc., for Langley Research Center.Cover title.Inclu...
Helium penetration and spreading in Mach 2 airstream using delta wing injector.Includes bibliographi...
In this study, the mixture formation processes of high pressure hydrogen jets were investigated usin...
The following computational study examines the structure of sonic hydrogen jets using inlet conditio...
Prepared at Langley Research Center.N 71-34283.Includes bibliographical references (p. 33-34).Mode o...
Fuel injection parameter effects on mixing of gaseous hydrogen with supersonic air strea
Mixing of hydrogen downstream from multiple injectors normal to supersonic jet flow, for supersoni...
N69-32480."July 1969"--Cover.Includes bibliographical references (p. 42-44).Prepared by Johns Hopkin...
Effect of injectant molecular weight on mixing of normal jet in Mach 4 airstream - tables and graph
Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...
Turbulent mixing of compressible air in supersonic and subsonic coaxial jet flows.Includes bibliogra...
In pursuit of a more efficient and effective fuel-air mixing for a SCRAMjet combustor, this study in...
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected nor...
Prepared at Langley Research Center.N 71-34274.Includes bibliographical references (p. 14-15).Mode o...
Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...
Prepared by Fluid Mechanics and Thermal Systems, Inc., for Langley Research Center.Cover title.Inclu...
Helium penetration and spreading in Mach 2 airstream using delta wing injector.Includes bibliographi...
In this study, the mixture formation processes of high pressure hydrogen jets were investigated usin...
The following computational study examines the structure of sonic hydrogen jets using inlet conditio...
Prepared at Langley Research Center.N 71-34283.Includes bibliographical references (p. 33-34).Mode o...
Fuel injection parameter effects on mixing of gaseous hydrogen with supersonic air strea
Mixing of hydrogen downstream from multiple injectors normal to supersonic jet flow, for supersoni...
N69-32480."July 1969"--Cover.Includes bibliographical references (p. 42-44).Prepared by Johns Hopkin...
Effect of injectant molecular weight on mixing of normal jet in Mach 4 airstream - tables and graph
Issued April 1977.Prepared by Fluid Mechanics and Thermal Systems, Inc. for Langley Research Center ...
Turbulent mixing of compressible air in supersonic and subsonic coaxial jet flows.Includes bibliogra...
In pursuit of a more efficient and effective fuel-air mixing for a SCRAMjet combustor, this study in...