Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms

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ISBN 13 :
Total Pages : 128 pages
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Book Synopsis Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms by :

Download or read book Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms written by and published by . This book was released on 1999 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721087426
Total Pages : 126 pages
Book Rating : 4.0/5 (874 download)

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Book Synopsis Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms by : National Aeronautics and Space Administration (NASA)

Download or read book Investigation of Vortex Flaps and Other Flow Control Devices on Generic High-Speed Civil Transport Planforms written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-13 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: A parametric cranked delta planform study has been conducted in the Langley 14- by 22-Foot Subsonic Tunnel with the following objectives: (1) to evaluate the vortex flap design methodology for cranked delta wings, (2) to determine the influence of leading-edge sweep and the outboard wing on vortex flap effectiveness, (3) to evaluate novel flow control concepts, and (4) to validate unstructured grid Euler computer code predictions with modeled vortex and trailing-edge flaps. Two families of cranked delta planforms were investigated. One family had constant aspect ratio, while the other had a constant nondimensional semispan location of the leading-edge break. The inboard leading-edge sweep of the planforms was varied between 68 deg., 71 deg., and 74 deg., while outboard leading-edge sweep was varied between 48 deg. and 61 deg. Vortex flaps for the different planforms were designed by an analytical vortex flap design method. The results indicate that the effectiveness of the vortex flaps was only slightly influenced by the variations in the parametric planforms. The unstructured grid Euler computer code was successfully used to model the configurations with vortex flaps. The vortex trap concept was successfully demonstrated. Kjerstad, Kevin J. and Campbell, Bryan A. and Gile, Brenda E. and Kemmerly, Guy T. Langley Research Center RTOP 537-03-22-02

NASA Langley Scientific and Technical Information Output: 1999

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ISBN 13 :
Total Pages : 182 pages
Book Rating : 4.:/5 (317 download)

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Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 576 pages
Book Rating : 4.3/5 (243 download)

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Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 836 pages
Book Rating : 4.:/5 (31 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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International Aerospace Abstracts

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ISBN 13 :
Total Pages : 530 pages
Book Rating : 4.3/5 (91 download)

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Innovation in Flight

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ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Innovation in Flight by : Joseph R. Chambers

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Aeronautical Technologies for the Twenty-first Century

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ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (269 download)

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Book Synopsis Aeronautical Technologies for the Twenty-first Century by : National Research Council (U.S.). Committee on Aeronautical Technologies

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 287)

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ISBN 13 :
Total Pages : 706 pages
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 287) by :

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NASA SP.

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ISBN 13 :
Total Pages : 654 pages
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A Strategy for Electronic Dissemination of NASA Langley Technical Publications

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ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.:/5 (317 download)

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Introduction to Aircraft Flight Mechanics

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Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)

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Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

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:

Aeroacoustics of Flight Vehicles

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ISBN 13 :
Total Pages : 620 pages
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Book Synopsis Aeroacoustics of Flight Vehicles by : Harvey H. Hubbard

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Elegance in Flight

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ISBN 13 : 9781626830226
Total Pages : 328 pages
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Book Synopsis Elegance in Flight by : Albert C. Piccirillo

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography

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ISBN 13 :
Total Pages : 516 pages
Book Rating : 4.:/5 (317 download)

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Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography written by and published by . This book was released on 1988 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt: