Effects of Radial and Circumferential Inlet Velocity Profile Distortions on Performance of a Short length Double annular Ram induction Combustor

Effects of Radial and Circumferential Inlet Velocity Profile Distortions on Performance of a Short length Double annular Ram induction Combustor
Author: Donald F. Schultz
Publsiher: Unknown
Total Pages: 52
Release: 1972
Genre: Aircraft gas-turbines
ISBN: UIUC:30112106883959

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Inlet air velocity profile tests were conducted on a full-scale short-length 102-centimeter-diameter annual combustor designed for advanced gas turbine engine applications. The inlet profiles studied include radial distortions that were center peaked, and tip peaked, as well as a circumferential distortion which was center peaked for one-third of the circumference and flat for the other two-thirds. An increase in combustor pressure loss was the most significant effect of the radial air velocity distortions. With the circumferential distortion, exit temperature pattern factor doubled when compared to a flat velocity profile.

NASA Technical Note

NASA Technical Note
Author: Anonim
Publsiher: Unknown
Total Pages: 382
Release: 1975
Genre: Electronic Book
ISBN: MINN:31951000846529V

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NASA Technical Memorandum

NASA Technical Memorandum
Author: Anonim
Publsiher: Unknown
Total Pages: 542
Release: 1974
Genre: Aeronautics
ISBN: MINN:31951000844871U

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Jet Engine Exhaust Emissions of High altitude Commercial Aircraft Projected to 1990

Jet Engine Exhaust Emissions of High altitude Commercial Aircraft Projected to 1990
Author: Jack Grobman,Robert D. Ingebo
Publsiher: Unknown
Total Pages: 90
Release: 1974
Genre: Air
ISBN: UIUC:30112106615047

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Inventory of Current Energy Research and Development

Inventory of Current Energy Research and Development
Author: Oak Ridge National Laboratory
Publsiher: Unknown
Total Pages: 1296
Release: 1972
Genre: Electric power distribution
ISBN: UIUC:30112009021483

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pt III and IV

pt  III and IV
Author: Oak Ridge National Laboratory
Publsiher: Unknown
Total Pages: 508
Release: 1974
Genre: Electric power distribution
ISBN: SRLF:A0000142349

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author: Anonim
Publsiher: Unknown
Total Pages: 1038
Release: 1972
Genre: Aeronautics
ISBN: UIUC:30112032440452

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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.

Aircraft Engines and Gas Turbines second edition

Aircraft Engines and Gas Turbines  second edition
Author: Jack L. Kerrebrock
Publsiher: MIT Press
Total Pages: 497
Release: 1992-04-22
Genre: Technology & Engineering
ISBN: 9780262534031

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Aircraft Engines and Gas Turbines is widely used as a text in the United States and abroad, and has also become a standard reference for professionals in the aircraft engine industry. Unique in treating the engine as a complete system at increasing levels of sophistication, it covers all types of modern aircraft engines, including turbojets, turbofans, and turboprops, and also discusses hypersonic propulsion systems of the future. Performance is described in terms of the fluid dynamic and thermodynamic limits on the behavior of the principal components: inlets, compressors, combustors, turbines, and nozzles. Environmental factors such as atmospheric pollution and noise are treated along with performance. This new edition has been substantially revised to include more complete and up-to-date coverage of compressors, turbines, and combustion systems, and to introduce current research directions. The discussion of high-bypass turbofans has been expanded in keeping with their great commercial importance. Propulsion for civil supersonic transports is taken up in the current context. The chapter on hypersonic air breathing engines has been expanded to reflect interest in the use of scramjets to power the National Aerospace Plane. The discussion of exhaust emissions and noise and associated regulatory structures have been updated and there are many corrections and clarifications.