The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Basic Results For Slotted Configuration
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The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Basic Results For Slotted Configuration
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Author :
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Basic Results For Slotted Configuration written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher:
Release Date : 2018-11-14
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by National Aeronautics and Space Adm Nasa and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-11-14 with categories.
The effects of Mach number and Reynolds number on the experimental surface pressure distributions and transition patterns for a large chord, swept supercritical airfoil incorporating an active Laminar Flow Control suction system with spanwise slots are presented. The experiment was conducted in the Langley 8 foot Transonic Pressure Tunnel. Also included is a discussion of the influence of model/tunnel liner interactions on the airfoil pressure distribution. Mach number was varied from 0.40 to 0.82 at two chord Reynolds numbers, 10 and 20 x 1,000,000, and Reynolds number was varied from 10 to 20 x 1,000,000 at the design Mach number. Harris, Charles D. and Brooks, Cuyler W., Jr. and Clukey, Patricia G. and Stack, John P. Langley Research Center BOUNDARY LAYER CONTROL; LAMINAR FLOW; SUPERCRITICAL AIRFOILS; SWEPT WINGS; TRANSONIC FLOW; WING SLOTS; COMPUTATIONAL FLUID DYNAMICS; INTERACTIONAL AERODYNAMICS; MACH NUMBER; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; SUCTION; WIND TUNNEL TESTS...
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author : Charles D. Harris
language : en
Publisher:
Release Date : 1988
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by Charles D. Harris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Aerodynamics, Transonic categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author :
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aerofoils categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author : Cuyler W. Brooks
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by Cuyler W. Brooks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Evaluation Of Initial Perforated Configuration
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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2018-11-14
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Evaluation Of Initial Perforated Configuration written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-11-14 with Science categories.
The initial evaluation of a large-chord, swept, supercritical airfoil incorporating an active laminar-flow-control (LFC) suction system with a perforated upper surface is documented in a chronological manner, and the deficiencies in the suction capability of the perforated panels as designed are described. The experiment was conducted in the Langley 8-Foot Transonic Pressure Tunnel. Also included is an evaluation of the influence of the proximity of the tunnel liner to the upper surface of the airfoil pressure distribution. Harris, Charles D. and Brooks, Cuyler W., Jr. and Clukey, Patricia G. and Stack, John P. Langley Research Center AIRFOILS; BOUNDARY LAYER CONTROL; LAMINAR BOUNDARY LAYER; LAMINAR FLOW; SUPERCRITICAL WINGS; SWEPT WINGS; TRANSONIC FLOW; WIND TUNNEL TESTS; PRESSURE DISTRIBUTION; SUCTION; TRANSONIC WIND TUNNELS...
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author : Charles D. Harris
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by Charles D. Harris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author :
language : en
Publisher:
Release Date : 1992
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aerodynamics, Transonic categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Author : Cuyler W. Brooks
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil written by Cuyler W. Brooks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aerodynamics, Transonic categories.
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Drag Equations
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Author :
language : en
Publisher:
Release Date : 1989
The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil Drag Equations written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.