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Book Technical Memorandum PIB

Download or read book Technical Memorandum PIB written by and published by . This book was released on 1948 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Compressible Laminar Boundary Layer with Fluid Injection

Download or read book The Compressible Laminar Boundary Layer with Fluid Injection written by George M. Low and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A solution of the equations of the compressible laminar boundary layer including the effects of transpiration cooling is presented. The analysis applies to the flow over an isothermal porous plate with a velocity of fluid injection proportional to the reciprocal of the square root of the distance from the leading edge.

Book U S  Government Research Reports

Download or read book U S Government Research Reports written by and published by . This book was released on 1961 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book AFOSR

    Book Details:
  • Author : United States. Air Force. Office of Scientific Research
  • Publisher :
  • Release : 1950
  • ISBN :
  • Pages : 1190 pages

Download or read book AFOSR written by United States. Air Force. Office of Scientific Research and published by . This book was released on 1950 with total page 1190 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Heat Transfer

    Book Details:
  • Author : James M. Jacobs
  • Publisher :
  • Release : 1957
  • ISBN :
  • Pages : 180 pages

Download or read book Heat Transfer written by James M. Jacobs and published by . This book was released on 1957 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Analysis of Turbulent Boundary Layers

Download or read book Analysis of Turbulent Boundary Layers written by Tuncer Cebeci and published by Elsevier. This book was released on 2012-12-02 with total page 423 pages. Available in PDF, EPUB and Kindle. Book excerpt: Analysis of Turbulent Boundary Layers focuses on turbulent flows meeting the requirements for the boundary-layer or thin-shear-layer approximations. Its approach is devising relatively fundamental, and often subtle, empirical engineering correlations, which are then introduced into various forms of describing equations for final solution. After introducing the topic on turbulence, the book examines the conservation equations for compressible turbulent flows, boundary-layer equations, and general behavior of turbulent boundary layers. The latter chapters describe the CS method for calculating two-dimensional and axisymmetric laminar and turbulent boundary layers. This book will be useful to readers who have advanced knowledge in fluid mechanics, especially to engineers who study the important problems of design.

Book Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1955
  • ISBN :
  • Pages : 34 pages

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book TID

Download or read book TID written by and published by . This book was released on 1957 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Air Force Scientific Research Bibliography  1950 56

Download or read book Air Force Scientific Research Bibliography 1950 56 written by Library of Congress. Science and Technology Division and published by . This book was released on 1961 with total page 1196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1973 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-10 with total page 1540 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note

Download or read book Technical Note written by and published by . This book was released on 1955 with total page 386 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index to PB Reports Listed in U S  Government Research Reports

Download or read book Index to PB Reports Listed in U S Government Research Reports written by and published by . This book was released on 1958 with total page 472 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note   National Advisory Committee for Aeronautics

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 988 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Skin Friction and Heat Transfer Characteristics of the Compressible Laminar Boundary Layer with Injection of a Light  Medium  and Heavy Gas

Download or read book Skin Friction and Heat Transfer Characteristics of the Compressible Laminar Boundary Layer with Injection of a Light Medium and Heavy Gas written by L. M. Albacete and published by . This book was released on 1967 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of the injection of a light, medium, and heavy gas on the skin friction and heat transfer characteristics of the laminar boundary layer flow over a flat plate were investigated. This was done by a numerical solution of the governing differential equations for injection rate parameters of -0, -0. 1, -0.2; Mach numers from 0 to 3; and wall-to-stream temperature ratios of 0.25, 0.50, and 1.00. The results show that the selection of discrete injection systems must represent a favorable compromise between conflicting factors (such as small molecular weight and large molecular diameters) which influence the amount of reduction in skin friction and heat transfer desired.