NASA Technical Note PDF Download
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Author:
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Category :
Languages : en
Pages : 826
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Author:
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ISBN:
Category :
Languages : en
Pages : 826
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Author:
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ISBN:
Category : Astronautics
Languages : en
Pages : 724
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Author: Lucille C. Geyser
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 212
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 826
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Author: James F. Sellers
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 212
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Author: Vassil N. Alexandrov
Publisher: Springer
ISBN: 3540455450
Category : Computers
Languages : en
Pages : 1294
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Book Description
LNCS volumes 2073 and 2074 contain the proceedings of the International Conference on Computational Science, ICCS 2001, held in San Francisco, California, May 27 -31, 2001. The two volumes consist of more than 230 contributed and invited papers that reflect the aims of the conference to bring together researchers and scientists from mathematics and computer science as basic computing disciplines, researchers from various application areas who are pioneering advanced application of computational methods to sciences such as physics, chemistry, life sciences, and engineering, arts and humanitarian fields, along with software developers and vendors, to discuss problems and solutions in the area, to identify new issues, and to shape future directions for research, as well as to help industrial users apply various advanced computational techniques.
Author:
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ISBN:
Category : Science
Languages : en
Pages : 818
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Author: Monte Ung
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ISBN:
Category : Aeronautics
Languages : en
Pages : 248
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Author: Robert W. Koenig
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 172
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A computer program titled GENENG is described. The program uses component performance maps to enable the user to do analytical steady-state engine cycle calculations. Through a scaling procedure, each of the component maps can be used to represent a family of maps (different design values of pressure ratios, efficiency, weight flow, etc. ). Either convergent or convergent divergent nozzles may be used. Included is a complete FORTRAN IV listing of the program. Sample results and input explanations are shown for one-spool and two-spool turbojets and two-spool separate and mixed-flow turbofans operating at design and off-design conditions. The computer program is available from the authors.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 852
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