Add to ORKGCombustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Prepared at Lewis Research Center."October 1969."Cover title.Includes bibliographical references (p. 27).Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Mode of access: Internet
Thermodynamic and transport properties of air, and combustion products of natural gas and air, and j...
Prepared for NASA under contract no. NASW-2075 by Advanced Technology Laboratories."February 1972."C...
A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor module...
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fue
Performance of turbojet swirl module combustor segment at high temperatures.Prepared at Lewis Resear...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...
Prepared at Lewis Research Center.N69-16154.Cover title.Includes bibliographical references (p. 25)....
Prepared at Lewis Research Center."August 1959."Cover title.Includes bibliographical references (p. ...
STAR category no. 20."August 1979"--Cover.Includes bibliographical references.Mode of access: Intern...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ac...
Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Prepared by Lewis Research Center."November 1971."--Cover.Major NASA subject terms: Combustion chamb...
Thermodynamic and transport properties of air, and combustion products of natural gas and air, and j...
Prepared for NASA under contract no. NASW-2075 by Advanced Technology Laboratories."February 1972."C...
A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor module...
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fue
Performance of turbojet swirl module combustor segment at high temperatures.Prepared at Lewis Resear...
Combustion stability limits for swirl-jet combustor modules combining air swirl and impinging jet at...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...
Prepared at Lewis Research Center.N69-16154.Cover title.Includes bibliographical references (p. 25)....
Prepared at Lewis Research Center."August 1959."Cover title.Includes bibliographical references (p. ...
STAR category no. 20."August 1979"--Cover.Includes bibliographical references.Mode of access: Intern...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ac...
Prepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes...
Stability limits and efficiency of swirl can combustor modules burning natural gas fue
Prepared by Lewis Research Center."November 1971."--Cover.Major NASA subject terms: Combustion chamb...
Thermodynamic and transport properties of air, and combustion products of natural gas and air, and j...
Prepared for NASA under contract no. NASW-2075 by Advanced Technology Laboratories."February 1972."C...
A 27-inch (68.6-cm) long rectangular combustor segment consisting of an array of 48 combustor module...