Author: Jerrold D. WearPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engine.
Tests of a Full-scale Annular Ram-induction Combustor for a Mach 3 Cruise Turbojet Engine
Author: Jerrold D. WearPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engine.
Proceedings of the Third Conference on the Climatic Impact Assessment Program
Author: Anthony J. BroderickPublisher:
ISBN:
Category : Aerosols
Languages : en
Pages : 684
Book Description
Aeronautical Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
NASA Technical Note
Author: Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Effect of Exit Temperature Sampling Density on Measured Combustor Performance
Author: Robert E. JonesPublisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 12
Book Description
Sampling point decrease effects on computed annular combustor parameters and exhaust nozzle temperature profile analysis of thermocouple location.
Comparison of Simplex and Dual-orifice Fuel Nozzles with Ambient and Heated Fuel in an Annular Turbojet Combustor
Author: Donald F. SchultzPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
A full-scale annular combustor was operated with simplex fuel nozzles of three flow ranges and with dual-orifice fuel nozzles. The dual-orifice nozzles provided combustion efficiencies within 2 to 3 percent of the peak values obtained with any of the simplex atomizers. A wide range of operating conditions including altitude relight, simulated takeoff, Mach 2.7 cruise, and Mach 3.0 cruise were studied. Measurements were made of combustion efficiency, pattern factor , flame radiation, smoke emission, and response to rapid increase in fuel flow. Fuel heated to 300 [degree] F (423 K) was used in many of the tests; heated fuel usually increased combustion efficiency.
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1348
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Book Description
Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1730
Book Description