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The Nasa Langley Laminar Flow Control Experiment On A Swept Supercritical Airfoil
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Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil: Basic Results for Slotted Configuration by :
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil: Basic Results for Slotted Configuration written by and published by . This book was released on 1989 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by :
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by and published by . This book was released on 1992 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Charles D. Harris
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Charles D. Harris and published by . This book was released on 1988 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Cuyler W. Brooks
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Cuyler W. Brooks and published by . This book was released on 1989 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Cuyler W. Brooks
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Cuyler W. Brooks and published by . This book was released on 1989 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-Flow-Control Experiment on a Swept Supercritical Airfoil by : National Aeronautics and Space Adm Nasa
Download or read book The NASA Langley Laminar-Flow-Control Experiment on a Swept Supercritical Airfoil written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-14 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723447761 Total Pages :126 pages Book Rating :4.4/5 (477 download)
Book Synopsis The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil by : National Aeronautics and Space Administration (NASA)
Download or read book The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781731325471 Total Pages :128 pages Book Rating :4.3/5 (254 download)
Book Synopsis The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil: Evaluation of Initial Perforated Configuration by : National Aeronautics and Space Adm Nasa
Download or read book 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 published by Independently Published. This book was released on 2018-11-14 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722873516 Total Pages :42 pages Book Rating :4.8/5 (735 download)
Book Synopsis The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil - Drag Equations by : National Aeronautics and Space Administration (NASA)
Download or read book The NASA Langley Laminar-Flow-Control Experiment on a Swept, Supercritical Airfoil - Drag Equations written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-13 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Langley Research Center has designed a swept, supercritical airfoil incorporating Laminar Flow Control for testing at transonic speeds. Analytical expressions have been developed and an evaluation made of the experimental section drag, composed of suction drag and wake drag, using theoretical design information and experimental data. The analysis shows that, although the sweep-induced boundary-layer crossflow influence on the wake drag is too large to be ignored and there is not a practical method for evaluating these crossflow effects on the experimental wake data, the conventional unswept 2-D wake-drag computation used in the reduction of the experimental data is at worst 10 percent too high. Brooks, Cuyler W., Jr. and Harris, Charles D. and Harvey, William D. Langley Research Center RTOP 505-60-31-03...
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil: Suction Coefficient Analysis by :
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil: Suction Coefficient Analysis written by and published by . This book was released on 1991 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Cuyler W. Brooks (Jr.)
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Cuyler W. Brooks (Jr.) and published by . This book was released on 1991 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil by :
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil written by and published by . This book was released on 1989 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Charles D. Harris
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Charles D. Harris and published by . This book was released on 1992 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil by : Charles D. Harris
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept Supercritical Airfoil written by Charles D. Harris and published by . This book was released on 1989 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil by : Charles D. Harris
Download or read book The NASA Langley Laminar-flow-control Experiment on a Swept, Supercritical Airfoil written by Charles D. Harris and published by . This book was released on 1992 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723492198 Total Pages :24 pages Book Rating :4.4/5 (921 download)
Book Synopsis Two Experimental Supercritical Laminar-Flow-Control Swept-Wing Airfoils by : National Aeronautics and Space Administration (NASA)
Download or read book Two Experimental Supercritical Laminar-Flow-Control Swept-Wing Airfoils written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two supercritical laminar-flow-control airfoils were designed for a large-chord swept-wing experiment in the Langley 8-Foot Transonic Pressure Tunnel where suction was provided through most of the model surface for boundary-layer control. The first airfoil was derived from an existing full-chord laminar airfoil by extending the trailing edge and making changes in the two lower-surface concave regions. The second airfoil differed from the first one in that it was designed for testing without suction in the forward concave region of the lower surface. Differences between the first airfoil and the one from which it was derived as well as between the first and second airfoils are discussed. Airfoil coordinates and predicted pressure distributions for the design normal Mach number of 0.755 and section lift coefficient of 0.55 are given for the three airfoils. Allison, Dennis O. and Dagenhart, J. Ray Langley Research Center NASA-TM-89073, NAS 1.15:89073 RTOP 505-60-21-02
Book Synopsis The NASA Langley Laminar-flow-control Exp. on a Swept, Supercritical Airfoil by :
Download or read book The NASA Langley Laminar-flow-control Exp. on a Swept, Supercritical Airfoil written by and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
