Author: Arthur L. Smith
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
Book Description
Performance of Pure Fuels in a Single J33 Combustor
Author: Arthur L. Smith
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
NASA Technical Note
Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 922
Book Description
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 922
Book Description
Research Memorandum
Effects of Fuel Nozzle Design on Performance of an Experimental Annular Combustor Using Natural Gas Fuel
Author: Jerrold D. Wear
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The nozzles were designed to provide either axial, angled, or radial fuel injection. Each fuel nozzle was evaluated by measuring combustion efficiency at relatively severe combustor operating conditions. Combustor blowout and altitude ignition tests were also used to evaluate nozzle designs. Results indicate that angled injection gave higher combustion efficiency, less tendency toward combustion instability, and altitude relight characteristics equal to or superior to those of the other fuel nozzles that were tested.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The nozzles were designed to provide either axial, angled, or radial fuel injection. Each fuel nozzle was evaluated by measuring combustion efficiency at relatively severe combustor operating conditions. Combustor blowout and altitude ignition tests were also used to evaluate nozzle designs. Results indicate that angled injection gave higher combustion efficiency, less tendency toward combustion instability, and altitude relight characteristics equal to or superior to those of the other fuel nozzles that were tested.
NACA Research Memorandum
Comparison of Combustion Characteristics of ASTM A-1, Propane, and Natural-gas Fuels in an Annular Turbojet Combustor
Author: Jerrold D. Wear
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description