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Author: Paul W. Adam Publisher: ISBN: Category : Air-engines Languages : en Pages : 36
Book Description
A test facility for conducting full-scale advanced annular jet engine combustor research and durability tests is described. Combustors have been operated on ambient or heated ASTM-A1, natural gas, and propane fuels to an average exit temperature of 2400' F (1589 K). The airflow of 285 lb/sec (129.4 kg/sec) at 1200' F (922 K), 115 psia (79.2 N/cm2), and 60 000-ft (18 240-m) altitude exhaust capability allows simulation of combustor inlet conditions over most of the range of interest in supersonic cruise engines. Description of a unique jet-engine-fired, nonvitiating air heater is included. The test section, the instrumentation, the data acquisition system, and operation techniques and experiences are also described.
Author: Paul W. Adam Publisher: ISBN: Category : Air-engines Languages : en Pages : 36
Book Description
A test facility for conducting full-scale advanced annular jet engine combustor research and durability tests is described. Combustors have been operated on ambient or heated ASTM-A1, natural gas, and propane fuels to an average exit temperature of 2400' F (1589 K). The airflow of 285 lb/sec (129.4 kg/sec) at 1200' F (922 K), 115 psia (79.2 N/cm2), and 60 000-ft (18 240-m) altitude exhaust capability allows simulation of combustor inlet conditions over most of the range of interest in supersonic cruise engines. Description of a unique jet-engine-fired, nonvitiating air heater is included. The test section, the instrumentation, the data acquisition system, and operation techniques and experiences are also described.
Author: Jack D. Mattingly Publisher: AIAA ISBN: 9781600860164 Category : Aircraft gas-turbines Languages : en Pages : 732
Book Description
Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 380
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.
Author: National Research Council (U.S.). Committee on Turbine Engine Test Facilities Publisher: National Academies ISBN: Category : Gas-turbines Languages : en Pages : 52
Author: Mario Asselin Publisher: American Institute of Aeronautics and Astronautics Incorporated ISBN: 9781624105920 Category : Airplanes Languages : en Pages : 0
Book Description
Serves as a single source reference, from the basic theory to practical cases, for certification flight testing and operational performance monitoring. The book provides more real-life examples than are offered in traditional textbooks.
Author: United States. Congress. House. Committee on Appropriations. Subcommittee on Department of Defense Publisher: ISBN: Category : United States Languages : en Pages : 782
Author: Paul W. Adam
Author: Paul W. Adam
Author: Jack D. Mattingly
Author: Frank K. Lu
Author: 
Author: National Research Council (U.S.). Committee on Turbine Engine Test Facilities
Author: Defense Documentation Center (U.S.)
Author: North Atlantic Treaty Organization. Combustion and Propulsion Panel
Author: Mario Asselin
Author: 
Author: United States. Congress. House. Committee on Appropriations. Subcommittee on Department of Defense