Natural Laminar Flow Experiments On Modern Airplane Surfaces

Natural Laminar Flow Experiments On Modern Airplane Surfaces Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Natural Laminar Flow Experiments On Modern Airplane Surfaces book. This book definitely worth reading, it is an incredibly well-written.

Natural Laminar Flow and Laminar Flow Control

Author : R.W. Barnwell,M.Y. Hussaini
Publisher : Springer Science & Business Media
Page : 415 pages
File Size : 53,9 Mb
Release : 2012-12-06
Category : Science
ISBN : 9781461228721

Get Book

Natural Laminar Flow and Laminar Flow Control by R.W. Barnwell,M.Y. Hussaini Pdf

Research on laminar flow and its transition to turbulent flow has been an important part of fluid dynamics research during the last sixty years. Since transition impacts, in some way, every aspect of aircraft performance, this emphasis is not only understandable but should continue well into the future. The delay of transition through the use of a favorable pressure gradient by proper body shaping (natural laminar flow) or the use of a small amount of suction (laminar flow control) was recognized even in the early 1930s and rapidly became the foundation of much of the laminar flow research in the U.S. and abroad. As one would expect, there have been many approaches, both theoretical and experimental, employed to achieve the substantial progress made to date. Boundary layer stability theories have been formu lated and calibrated by a good deal of wind tunnel and flight experiments. New laminar now airfoils and wings have been designed and many have been employed in aircraft designs. While the early research was, of necessity, concerned with the design of subsonic aircraft interest has steadily moved to higher speeds including those appropriate to planetary entry. Clearly, there have been substantial advances in our understanding of transition physics and in the development and application of transition prediction methodolo gies to the design of aircraft.

Laminar Flow Aircraft Certification

Author : Anonim
Publisher : Unknown
Page : 340 pages
File Size : 50,8 Mb
Release : 1986
Category : Fluid dynamics
ISBN : NASA:31769000467590

Get Book

Laminar Flow Aircraft Certification by Anonim Pdf

NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 142 pages
File Size : 52,8 Mb
Release : 1987
Category : Science
ISBN : STANFORD:36105024769460

Get Book

NASA Technical Paper by Anonim Pdf

New Results in Numerical and Experimental Fluid Mechanics X

Author : Andreas Dillmann,Gerd Heller,Ewald Krämer,Claus Wagner,Christian Breitsamter
Publisher : Springer
Page : 897 pages
File Size : 47,8 Mb
Release : 2016-03-28
Category : Technology & Engineering
ISBN : 9783319272795

Get Book

New Results in Numerical and Experimental Fluid Mechanics X by Andreas Dillmann,Gerd Heller,Ewald Krämer,Claus Wagner,Christian Breitsamter Pdf

This book presents contributions to the 19th biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. Though the book’s primary emphasis is on the aerospace context, it also addresses further important applications, e.g. in ground transportation and energy.

Design and Experimental Results for a Natural-Laminar-Flow Airfoil for General Aviation Application

Author : Dan M. Somers
Publisher : Unknown
Page : 108 pages
File Size : 44,9 Mb
Release : 1981
Category : Aerofoils
ISBN : UIUC:30112106670703

Get Book

Design and Experimental Results for a Natural-Laminar-Flow Airfoil for General Aviation Application by Dan M. Somers Pdf

A natural-laminar-flow airfoil for general aviation applications, the NLF(1)-0416, was designed and analyzed theoretically and verified experimentally in the Langley Low-Turbulence Pressure Tunnel. The basic objective of combining the high maximum lift of the NASA low-speed airfoils with the low cruise drag of the NACA 6-series airfoils was achieved. The safety requirement that the maximum lift coefficient not be significantly affected with transition fixed near the leading edge was also met. Comparisons of the theoretical and experimental results show excellent agreement. Comparisons with other airfoils, both laminar flow and turbulent flow, confirm the achievement of the basic objective.

Monthly Catalog of United States Government Publications

Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 128 pages
File Size : 50,5 Mb
Release : 1985
Category : Government publications
ISBN : WISC:89013738190

Get Book

Monthly Catalog of United States Government Publications by United States. Superintendent of Documents Pdf

February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

Basic Aerodynamics

Author : Gary A. Flandro,Howard M. McMahon,Robert L. Roach
Publisher : Cambridge University Press
Page : 433 pages
File Size : 41,9 Mb
Release : 2011-11-14
Category : Technology & Engineering
ISBN : 9781139498616

Get Book

Basic Aerodynamics by Gary A. Flandro,Howard M. McMahon,Robert L. Roach Pdf

In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.

Design and Experimental Results for a Flapped Natural-laminar-flow Airfoil for General Aviation Applications

Author : Dan M. Somers
Publisher : Unknown
Page : 132 pages
File Size : 50,7 Mb
Release : 1981
Category : Aerofoils
ISBN : UIUC:30112008638907

Get Book

Design and Experimental Results for a Flapped Natural-laminar-flow Airfoil for General Aviation Applications by Dan M. Somers Pdf

A flapped natural laminar flow airfoil for general aviation applications, the NLF(1)-0215F, has been designed and analyzed theoretically and verified experimentally in the Langley Low Turbulence Pressure Tunnel. The basic objective of combining the high maximum lift of the NASA low speed airfoils with the low cruise drag of the NACA 6 series airfoils has been achieved. The safety requirement that the maximum lift coefficient not be significantly affected with transition fixed near the leading edge has also been met. Comparisons of the theoretical and experimental results show generally good agreement.