Altitude Performance Investigation of Single- and Double-annular Turbojet-engine Combustors with Various Size Fuel Nozzles
Author: James L. Jr Harp
Publisher:
Published: 1952
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: James L. Jr Harp
Publisher:
Published: 1952
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKAuthor: Adam E. Sobolewski
Publisher:
Published: 1953
Total Pages: 46
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1959
Total Pages: 382
ISBN-13:
DOWNLOAD EBOOKAuthor: Eugene V. Zettle
Publisher:
Published: 1950
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1957
Total Pages: 860
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1957
Total Pages: 388
ISBN-13:
DOWNLOAD EBOOKAuthor: RIchard J. McCafferty
Publisher:
Published: 1948
Total Pages: 96
ISBN-13:
DOWNLOAD EBOOKAuthor: Richard J. McCafferty
Publisher:
Published: 1952
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1956
Total Pages: 716
ISBN-13:
DOWNLOAD EBOOKAuthor: J. Howard Childs
Publisher:
Published: 1947
Total Pages: 56
ISBN-13:
DOWNLOAD EBOOKThe combustion performance and particularly the phenomenon of altitude operational limits was studied by operating the annular combustor of a turbojet engine over a range of conditions of air flow, inlet pressure, inlet temperature, and fuel flow. The combustor investigated was not the latest version of this combustor and the data are presented primarily because they are indicative of general trends and phenomena that apply to a large class of turbojet combustors.