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Investigation Of Vortex Flaps And Other Flow Control Devices On Generic High Speed Civil Transport Planforms
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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:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721087426 Total Pages :126 pages Book Rating :4.0/5 (874 download)
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
Book Synopsis NASA Langley Scientific and Technical Information Output: 1999 by :
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Author :National Research Council (U.S.). Committee on Aeronautical Technologies Publisher : ISBN 13 : Total Pages :21 pages Book Rating :4.:/5 (269 download)
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 287) by :
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography by :
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