Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1977 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Supercritical Airfoils written by Charles D. Harris and published by . This book was released on 1990 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Supercritical Airfoils written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented. Harris, Charles D. Langley Research Center...

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:

Download or read book NASA SC 2 0714 Airfoil Data Corrected for Sidewall Boundary layer Effects in the Langley 0 3 meter Transonic Cryogenic Tunnel written by Renaldo V. Jenkins and published by . This book was released on 1989 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Two dimensional Wind tunnel Tests of a NASA Supercritical Airfoil with Various High lift Systems Volume 1 Data Analysis written by E. Omar and published by . This book was released on 1977 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of Effects of Trailing edge Geometry on a NASA Supercritical Airfoil Section written by Charles D. Harris and published by . This book was released on 1971 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1971 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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...

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 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Two dimensional Wind tunnel Tests of a NASA Supercritical Airfoil with Various High lift Systems Volume 2 Test Data written by and published by . This book was released on 1977 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development of Two Supercritical Airfoils with a Thickness to chord Ratio of 0 20 and Design Lift Coefficients of 0 3 and 0 4 written by and published by . This book was released on 1976 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Transonic wind tunnel investigation of the maneuver potential of the NASA supercritical wing concept written by James B. Hallissy and published by . This book was released on 1977 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The NASA Supercritical wing Technology written by and published by . This book was released on 1978 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Detailed Transonic Flow Field Measurements about a Supercritical Airfoil Section written by and published by . This book was released on 1975 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Aerodynamic Characteristics of a 14 percent thick NASA Phase 2 Supercritical Airfoil Designed for a Lift Coefficient of 0 7 written by Charles D. Harris and published by . This book was released on 1980 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: