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Author : W.E. Gray
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book A Laminar Flow Experiment in Flight on a Swept Wing (A.W.52) written by W.E. Gray and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. A. Rozendaal
Publisher :
ISBN 13 :
Total Pages : 114 pages
Book Rating : 4.F/5 ( download)
Download or read book Natural Laminar Flow Flight Experiments on a Swept Wing Business Jet written by R. A. Rozendaal and published by . This book was released on 1986 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download A History of Suction-type Laminar-flow Control with Empahsis [i.e. Emphasis] on Flight Research PDF Online Free](https://books.google.com/books/content/images/frontcover/mS4rAAAAIAAJ?fife=w200-h370)
Author : Albert L. Braslow
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.F/5 ( download)
Download or read book A History of Suction-type Laminar-flow Control with Empahsis [i.e. Emphasis] on Flight Research written by Albert L. Braslow and published by . This book was released on 1999 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)
Download or read book Selected Experiments in Laminar Flow: An Annotated Bibliography written by and published by . This book was released on 1992 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard G. Rhodes
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (69 download)
Download or read book Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research written by Richard G. Rhodes and published by . This book was released on 2010 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The high cost of energy has resulted in a renewed interest in the study of reducing skin-friction drag in aeronautical applications. Laminar Flow Control (LFC) refers to any technique which alters the basic-state flow-field to delay transition from laminar to turbulent flow. Achieving fully laminar flow over a civilian transport wing will significantly reduce drag and fuel costs while increasing range and performance. Boundary-layer suction has proven to be an effective means of achieving laminar flow over an aircraft wing as demonstrated with the Northrop X-21 program; however, even with the savings in fuel, the high manufacturing and maintenance costs have discouraged the use of this technology. Recent work using threedimensional (3-D) spanwise-periodic distributed roughness elements (DREs) has shown great promise as a means of controlling the crossflow instability responsible for transition over a swept wing without the need for a complex suction system. The Texas A.
Author :
Publisher :
ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.:/5 (317 download)
Download or read book Research in Natural Laminar Flow and Laminar-Flow Control, Part 1 written by and published by . This book was released on 1987 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Adm Nasa
Publisher :
ISBN 13 : 9781728841540
Total Pages : 36 pages
Book Rating : 4.8/5 (415 download)
Download or read book Wing Leading Edge Joint Laminar Flow Tests written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-10-17 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An F-104G aircraft at NASA's Dryden Flight Research Center has been equipped with a specially designed and instrumented test fixture to simulate surface imperfections of the type likely to be present near the leading edge on the wings of some laminar flow aircraft. The simulated imperfections consisted of five combinations of spanwise steps and gaps of various sizes. The unswept fixture yielded a pressure distribution similar to that of some laminar flow airfoils. The experiment was conducted at cruise conditions typical for business-jets and light transports: Mach numbers were in the range 0.5-0.8, and unit Reynolds numbers were 1.5-2.5 million per foot. Skin friction measurements indicated that laminar flow was often maintained for some distance downstream of the surface imperfections. Further work is needed to more precisely define transition location and to extend the experiments to swept-wing conditions and a broader range of imperfection geometries. Drake, Aaron and Westphal, Russell V. and Zuniga, Fanny A. and Kennelly, Robert A., Jr. and Koga, Dennis J. Ames Research Center RTOP 505-59-20...
Author : Philip P. Antonatos
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)
Download or read book Summary of Laminar Flow Control Techniques for Aircraft written by Philip P. Antonatos and published by . This book was released on 1964 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. R. Landeryou
Publisher :
ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (713 download)
Download or read book Flight Tests of a Laminar Flow Swept Wing with Boundary Layer Control by Suction written by R. R. Landeryou and published by . This book was released on 1964 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (317 download)
Download or read book Variable Sweep Transition Flight Experiment (VSTFE)-parametric Pressure Distribution Boundary Layer Stability Study and Wing Glove Design Task written by and published by . This book was released on 1986 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Variable Sweep Transition Flight Experiment (VSTFE) was initiated to establish a boundary-layer transition data base for laminar flow wing design. For this experiment, full-span upper-surface gloves will be fitted to a variable sweep F-14 aircraft. The results of two initial tasks are documented: a parametric pressure distribution/boundary-layer stability study and the design of an upper-surface glove for Mach 0.8. The first task was conducted to provide a data base from which wing-glove pressure distributions could be selected for glove designs. Boundary-layer stability analyses were conducted on a set of pressure distributions for various wing sweep angles, Mach numbers, and Reynolds number in the range of those anticipated for the flight-test program. The design procedure for the Mach 0.8 glove is described, and boundary-layer stability calculations and pressure distributions are presented both at design and off-design conditions. Also included is the analysis of the clean-up glove (smoothed basic wing) that will be flight-tested initially and the analysis of a Mach 0.7 glove designed at the NASA Langley Research Center.
Author : Charles D. Harris
Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)
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:
![Download A History of Suction-type Laminar-flow Control with Empahsis [i.e. Emphasis] on Flight Research PDF Online Free](https://books.google.com/books/content/images/frontcover/bMd6SBzgH9kC?fife=w200-h370)
Author : Albert L. Braslow
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (31 download)
Download or read book A History of Suction-type Laminar-flow Control with Empahsis [i.e. Emphasis] on Flight Research written by Albert L. Braslow and published by . This book was released on 1999 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Tapan K. Sengupta
Publisher : CRC Press
ISBN 13 : 1439879451
Total Pages : 522 pages
Book Rating : 4.4/5 (398 download)
Download or read book Instabilities of Flows and Transition to Turbulence written by Tapan K. Sengupta and published by CRC Press. This book was released on 2012-04-24 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book covers material ranging from classical hydrodynamic instability to contemporary research areas, including bluff body flow instability and mixed convection flows. It also examines applications in aerospace and other branches of engineering such as fluid mechanics. The author addresses classical material as well as new perspectives and presents comprehensive coverage of receptivity to complement the instability material. This book presents a concise, up-to-date treatment of theory and applications of viscous flow instability, providing both current knowledge and techniques.
Author :
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Flight Test of Laminar Flow Control Leading-edge Systems written by and published by . This book was released on 1983 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (317 download)
Download or read book High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment written by and published by . This book was released on 1999 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.0/5 ( download)
Download or read book AIAA 2nd Shear Flow Conference written by and published by . This book was released on 1989 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James R. Hansen
Publisher :
ISBN 13 :
Total Pages : 990 pages
Book Rating : 4.:/5 (327 download)
Download or read book The Wind and Beyond: The ascent of the airplane written by James R. Hansen and published by . This book was released on 2003 with total page 990 pages. Available in PDF, EPUB and Kindle. Book excerpt:
