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:
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Altitude Performance Investigation of Two Single-annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor with Various Combustor-inlet Air Pressure Profiles
Author: Adam E. Sobolewski
Publisher:
Published: 1953
Total Pages: 46
ISBN-13:
DOWNLOAD EBOOKIndex of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1959
Total Pages: 382
ISBN-13:
DOWNLOAD EBOOKSimulated Altitude Performance of Two Annular Combustors with Continuous Axial Openings for Admission of Primary Air
Author: Eugene V. Zettle
Publisher:
Published: 1950
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKIndex of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1957
Total Pages: 860
ISBN-13:
DOWNLOAD EBOOKA Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
Published: 1957
Total Pages: 388
ISBN-13:
DOWNLOAD EBOOKEffect of Fuels and Fuel-nozzle Characteristics on Performance of an Annular Combustor at Simulated Altitude Conditions
Author: RIchard J. McCafferty
Publisher:
Published: 1948
Total Pages: 96
ISBN-13:
DOWNLOAD EBOOKPerformance Comparisons of JFC-2 and MIL-F-5624A (JP-3) Fuels in Tubular and Annular Combustors
Author: Richard J. McCafferty
Publisher:
Published: 1952
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKResearch Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1956
Total Pages: 716
ISBN-13:
DOWNLOAD EBOOKEffect of Combustor-inlet Conditions on Performance of an Annular Turbojet Combustor
Author: 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.
