Steady and Transient Performance Prediction of Gas Turbine Engines Held in Cambridge, Massachusetts on 27-28 May 1992; in Neubiberg, Germany on 9-10 June 1992; and in Chatillon/Bagneux, France on 11-12 June 1992 (Prediction Des Performances Des Moteurs a Turbine a Gaz en Regimes Etabli Et Transitoire). PDF Download
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Author:
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ISBN:
Category :
Languages : en
Pages : 192
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Book Description
This Lecture Series covers topics of aero-thermodynamic performance prediction methods for gas turbine engines with respect to steady and transient operation. This includes advanced cycle calculation methods, also taking into account variable cycle engine types. A very important objective is the consideration of installation effects, i.e. Reynolds number and inlet distortions, as well as advanced control concepts for increasing engine surge margins. In addition to these topics, individual papers include practical considerations in designing the engine cycle, dynamic simulation, inlet distortion effects in aircraft propulsion system integration, smart engines, performance and health monitoring models. This Lecture Series, sponsored by the Propulsion and Energetics Panel of AGARD, has been implemented by the Consultant and Exchange Programme. Aerothermodynamics, Predictions, Gas turbine engines, Computerized.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
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Book Description
This Lecture Series covers topics of aero-thermodynamic performance prediction methods for gas turbine engines with respect to steady and transient operation. This includes advanced cycle calculation methods, also taking into account variable cycle engine types. A very important objective is the consideration of installation effects, i.e. Reynolds number and inlet distortions, as well as advanced control concepts for increasing engine surge margins. In addition to these topics, individual papers include practical considerations in designing the engine cycle, dynamic simulation, inlet distortion effects in aircraft propulsion system integration, smart engines, performance and health monitoring models. This Lecture Series, sponsored by the Propulsion and Energetics Panel of AGARD, has been implemented by the Consultant and Exchange Programme. Aerothermodynamics, Predictions, Gas turbine engines, Computerized.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1494
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Author: Xenia Klinger
Publisher:
ISBN: 9780662191384
Category : City planning
Languages : en
Pages : 79
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Author:
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ISBN:
Category :
Languages : en
Pages :
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Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Daniel Uziel
Publisher: McFarland
ISBN: 0786488794
Category : History
Languages : en
Pages : 313
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Book Description
During World War II, aviation was among the largest industrial branches of the Third Reich. About 40 percent of total German war production, and two million people, were involved in the manufacture of aircraft and air force equipment. Based on German records, Allied intelligence reports, and eyewitness accounts, this study explores the military, political, scientific and social aspects of Germany's wartime aviation industry: production, research and development, Allied attacks, foreign workers and slave labor, and daily life and working conditions in the factories. Testimony from Holocaust survivors who worked in the factories provides a compelling new perspective on the history of the Third Reich.
Author: S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using digital computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight and dimensions computed by digital computer programs.This standard is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier.
Author: Richard W. Siegel
Publisher: Springer Science & Business Media
ISBN: 9780792358541
Category : Technology & Engineering
Languages : en
Pages : 378
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Book Description
Timely information on scientific and engineering developments occurring in laboratories around the world provides critical input to maintaining the economic and technological strength of the United States. Moreover, sharing this information quickly with other countries can greatly enhance the productivity of scientists and engineers. These are some of the reasons why the National Science Foundation (NSF) has been involved in funding science and technology assessments comparing the United States and foreign countries since the early 1980s. A substantial number of these studies have been conducted by the World Technology Evaluation Center (WTEC) managed by Loyola College through a cooperative agreement with NSF. The National Science and Technology Council (NSTC), Committee on Technology's Interagency Working Group on NanoScience, Engineering and Technology (CT/IWGN) worked with WTEC to develop the scope of this Nanostucture Science and Technology report in an effort to develop a baseline of understanding for how to strategically make Federal nanoscale R&D investments in the coming years. The purpose of the NSTC/WTEC activity is to assess R&D efforts in other countries in specific areas of technology, to compare these efforts and their results to U. S. research in the same areas, and to identify opportunities for international collaboration in precompetitive research. Many U. S. organizations support substantial data gathering and analysis efforts focusing on nations such as Japan. But often the results of these studies are not widely available. At the same time, government and privately sponsored studies that are in the public domain tend to be "input" studies.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 304
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