Design Optimization of Natural Laminar Flow Bodies in Compressible Flow

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ISBN 13 :
Total Pages : 24 pages
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Book Synopsis Design Optimization of Natural Laminar Flow Bodies in Compressible Flow by : Simha S. Dodbele

Download or read book Design Optimization of Natural Laminar Flow Bodies in Compressible Flow written by Simha S. Dodbele and published by . This book was released on 1992 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design Optimization of Natural Laminar Flow Bodies in Compressible Flow

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722153588
Total Pages : 24 pages
Book Rating : 4.1/5 (535 download)

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Book Synopsis Design Optimization of Natural Laminar Flow Bodies in Compressible Flow by : National Aeronautics and Space Administration (NASA)

Download or read book Design Optimization of Natural Laminar Flow Bodies in Compressible Flow written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An optimization method has been developed to design axisymmetric body shapes such as fuselages, nacelles, and external fuel tanks with increased transition Reynolds numbers in subsonic compressible flow. The new design method involves a constraint minimization procedure coupled with analysis of the inviscid and viscous flow regions and linear stability analysis of the compressible boundary-layer. In order to reduce the computer time, Granville's transition criterion is used to predict boundary-layer transition and to calculate the gradients of the objective function, and linear stability theory coupled with the e(exp n)-method is used to calculate the objective function at the end of each design iteration. Use of a method to design an axisymmetric body with extensive natural laminar flow is illustrated through the design of a tiptank of a business jet. For the original tiptank, boundary layer transition is predicted to occur at a transition Reynolds number of 6.04 x 10(exp 6). For the designed body shape, a transition Reynolds number of 7.22 x 10(exp 6) is predicted using compressible linear stability theory coupled with the e(exp n)-method. Dodbele, Simha S. Unspecified Center NAS1-18585; RTOP 505-59-10-02...

Design Optimization of Natural Laminar Flow Bodies in Compressible Flow

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Design Optimization of Natural Laminar Flow Bodies in Compressible Flow by : Simha S. Dodbele

Download or read book Design Optimization of Natural Laminar Flow Bodies in Compressible Flow written by Simha S. Dodbele and published by . This book was released on 1993 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An optimization method has been developed to design axisymmetric body shapes such as fuselages, nacelles, and external fuel tanks with increased transition Reynolds numbers in subsonic compressible flow. The new design method involves a constraint minimization procedure coupled with analysis of the inviscid and viscous flow regions and linear stability analysis of the compressible boundary-layer. In order to reduce the computer time, Granville's transition criterion is used to predict boundary-layer transition and to calculate the gradients of the objective function, and linear stability theory coupled with the e(exp n)-method is used to calculate the objective function at the end of each design iteration. Use of a method to design an axisymmetric body with extensive natural laminar flow is illustrated through the design of a tiptank of a business jet. For the original tiptank, boundary layer transition is predicted to occur at a transition Reynolds number of 6.04 x 10(exp 6). For the designed body shape, a transition Reynolds number of 7.22 x 10(exp 6) is predicted using compressible linear stability theory coupled with the e(exp n)-method.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 584 pages
Book Rating : 4.:/5 (3 download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Collection of Technical Papers

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ISBN 13 :
Total Pages : 278 pages
Book Rating : 4.X/5 (4 download)

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Journal of Aircraft

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ISBN 13 :
Total Pages : 636 pages
Book Rating : 4.:/5 (318 download)

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Download or read book Journal of Aircraft written by and published by . This book was released on 1999 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Reference Publication

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ISBN 13 :
Total Pages : 984 pages
Book Rating : 4.:/5 (319 download)

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Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 984 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AIAA 28th Aerospace Sciences Meeting

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ISBN 13 :
Total Pages : 530 pages
Book Rating : 4.0/5 ( download)

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Download or read book AIAA 28th Aerospace Sciences Meeting written by and published by . This book was released on 1990 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 590 pages
Book Rating : 4.:/5 (319 download)

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Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 590 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AIAA Journal

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ISBN 13 :
Total Pages : 1184 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis AIAA Journal by : American Institute of Aeronautics and Astronautics

Download or read book AIAA Journal written by American Institute of Aeronautics and Astronautics and published by . This book was released on 2007 with total page 1184 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 974 pages
Book Rating : 4.F/5 ( download)

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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 974 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)

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Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Aeronautical Journal

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ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.3/5 (91 download)

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Download or read book The Aeronautical Journal written by and published by . This book was released on 1993 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300)

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ISBN 13 :
Total Pages : 686 pages
Book Rating : 4.:/5 (317 download)

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Proceedings of the ... Congress of the International Council of the Aeronautical Sciences

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ISBN 13 :
Total Pages : 1116 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Proceedings of the ... Congress of the International Council of the Aeronautical Sciences by : International Council of the Aeronautical Sciences. Congress

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Conceptual Aircraft Design

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Publisher : John Wiley & Sons
ISBN 13 : 1119500281
Total Pages : 1052 pages
Book Rating : 4.1/5 (195 download)

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Book Synopsis Conceptual Aircraft Design by : Ajoy Kumar Kundu

Download or read book Conceptual Aircraft Design written by Ajoy Kumar Kundu and published by John Wiley & Sons. This book was released on 2019-04-08 with total page 1052 pages. Available in PDF, EPUB and Kindle. Book excerpt: Provides a Comprehensive Introduction to Aircraft Design with an Industrial Approach This book introduces readers to aircraft design, placing great emphasis on industrial practice. It includes worked out design examples for several different classes of aircraft, including Learjet 45, Tucano Turboprop Trainer, BAe Hawk and Airbus A320. It considers performance substantiation and compliance to certification requirements and market specifications of take-off/landing field lengths, initial climb/high speed cruise, turning capability and payload/range. Military requirements are discussed, covering some aspects of combat, as is operating cost estimation methodology, safety considerations, environmental issues, flight deck layout, avionics and more general aircraft systems. The book also includes a chapter on electric aircraft design along with a full range of industry standard aircraft sizing analyses. Split into two parts, Conceptual Aircraft Design: An Industrial Approach spends the first part dealing with the pre-requisite information for configuring aircraft so that readers can make informed decisions when designing vessels. The second part devotes itself to new aircraft concept definition. It also offers additional analyses and design information (e.g., on cost, manufacture, systems, role of CFD, etc.) integral to conceptual design study. The book finishes with an introduction to electric aircraft and futuristic design concepts currently under study. Presents an informative, industrial approach to aircraft design Features design examples for aircraft such as the Learjet 45, Tucano Turboprop Trainer, BAe Hawk, Airbus A320 Includes a full range of industry standard aircraft sizing analyses Looks at several performance substantiation and compliance to certification requirements Discusses the military requirements covering some combat aspects Accompanied by a website hosting supporting material Conceptual Aircraft Design: An Industrial Approach is an excellent resource for those designing and building modern aircraft for commercial, military, and private use.

Government Reports Annual Index

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ISBN 13 :
Total Pages : 1204 pages
Book Rating : 4.:/5 (89 download)

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Download or read book Government Reports Annual Index written by and published by . This book was released on 1993 with total page 1204 pages. Available in PDF, EPUB and Kindle. Book excerpt: