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9781288910731 - Conceptual Design Oriented Wing Structural Analysis and Optimization by Lau, May Yuen (12 results)
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Condition: As New. Unread book in perfect condition.
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Conceptual Design Oriented Wing Structural Analysis and Optimization (Paperback or Softback)
Language: English
Published by Biblioscholar 3/12/2013, 2013
ISBN 10: 1288910738 ISBN 13: 9781288910731
Paperback or Softback. Condition: New. Conceptual Design Oriented Wing Structural Analysis and Optimization. Book.
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Conceptual Design Oriented Wing Structural Analysis and Optimization
Seller: Ria Christie Collections, Uxbridge, United Kingdom
Seller rating 5 out of 5 stars
£ 13.90
£ 11.98 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketCondition: New. In.
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Conceptual Design Oriented Wing Structural Analysis and Optimization
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
Condition: New.
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Conceptual Design Oriented Wing Structural Analysis and Optimization
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
Condition: As New. Unread book in perfect condition.
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Condition: New. KlappentextrnrnAirplane optimization has always been the goal of airplane designers. In the conceptual design phase, a designer s goal could be tradeoffs between maximum structural integrity, minimum aerodynamic drag, or maximum stability and co.
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PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Conceptual Design Oriented Wing Structural Analysis and Optimization
Language: English
Published by Biblioscholar Mär 2013, 2013
ISBN 10: 1288910738 ISBN 13: 9781288910731
Taschenbuch. Condition: Neu. Neuware - Airplane optimization has always been the goal of airplane designers. In the conceptual design phase, a designer's goal could be tradeoffs between maximum structural integrity, minimum aerodynamic drag, or maximum stability and control, many times achieved separately. Bringing all of these factors into an iterative preliminary design procedure was time consuming, tedious, and not always accurate. For example, the final weight estimate would often be based upon statistical data from past airplanes. The new design would be classified based on gross characteristics, such as number of engines, wingspan, etc., to see which airplanes of the past most closely resembled the new design. This procedure works well for conventional airplane designs, but not very well for new innovative designs. With the computing power of today, new methods are emerging for the conceptual design phase of airplanes. Using finite element methods, computational fluid dynamics, and other computer techniques, designers can make very accurate disciplinary-analyses of an airplane design. These tools are computationally intensive, and when used repeatedly, they consume a great deal of computing time. In order to reduce the time required to analyze a design and still bring together all of the disciplines (such as structures, aerodynamics, and controls) into the analysis, simplified design computer analyses are linked together into one computer program. These design codes are very efficient for conceptual design. The work in this thesis is focused on a finite element based conceptual design oriented structural synthesis capability (CDOSS) tailored to be linked into ACSYNT.
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Conceptual Design Oriented Wing Structural Analysis and Optimization
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
£ 14.60
£ 3.29 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketPAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Condition: New. Print on Demand pp. 84.
