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Book Three dimensional  Unsteady lift Problems in High speed Flight

Download or read book Three dimensional Unsteady lift Problems in High speed Flight written by Harvard Lomax and published by . This book was released on 1950 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of the build-u of lift on two- and three-dimensional wings flying at high speeds is discussed as a boundary-value problem for the classical wave equation. Kirchhoff's formula is applied so that the analysis is reduced, just as in the steady state, to an investigation of sources and doublets. Some simple applications of this method are considered, including the determination of the starting lift of a three-dimensional wing and the potential functions for some types of unsteady vortex motion.

Book Three dimensional Unsteady Lift Problems in High speed Flight

Download or read book Three dimensional Unsteady Lift Problems in High speed Flight written by Harvard Lomax and published by . This book was released on 1951 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: The indicial lift and pitching-moment coefficients are derived for flat-plate triangular wings at supersonic speeds. Coefficients are determined for angle-of-attack distributions corresponding to sinking and pitching wings. The wing with supersonic edges is completely analyzed, the wing with subsonic edges is partially analyzed; the solution in this case being completed for very narrow wings by an application of slender wing theory. In case of the supersonic edges, a comparison is made with known two-dimensional results and also with results for the same triangular wing in reversed flow.

Book Three Dimensional Unsteady Lift Problems in High Speed Flight The Triangular Wing

Download or read book Three Dimensional Unsteady Lift Problems in High Speed Flight The Triangular Wing written by and published by . This book was released on 1950 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of the build-up of lift on two- and three-dimensional wings flying at high speeds is discussed as a boundary-value problem for the classical wave equation. Kirchhoff's formula is applied so that the analysis is reduced, Just as in the steady state, to an investigation of sources' and doublets. Some simple applications of this method are considered, including the determination of the starting lift of a three- dimensional wing and the potential functions for some types of unsteady vortex motion.

Book Adventures in Research

Download or read book Adventures in Research written by Edwin Phelps Hartman and published by . This book was released on 1970 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1953
  • ISBN :
  • Pages : 534 pages

Download or read book Annual Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report   National Advisory Committee for Aeronautics

Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1948 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeroelasticity

Download or read book Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 1996-01-01 with total page 886 pages. Available in PDF, EPUB and Kindle. Book excerpt: Highly regarded text deals with aeroelasticity as well as underlying aerodynamic and structural tools. Topics include incompressible flow, flutter, model theory, and much more. Over 300 illustrations. 1955 edition.

Book Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1952
  • ISBN :
  • Pages : 78 pages

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report of the National Advisory Committee for Aeronautics

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 1200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Book Report

    Book Details:
  • Author :
  • Publisher :
  • Release : 1954
  • ISBN :
  • Pages : 900 pages

Download or read book Report written by and published by . This book was released on 1954 with total page 900 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 480 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Rectangular wind tunnel Blocking Corrections Using the Velocity ratio Method

Download or read book Rectangular wind tunnel Blocking Corrections Using the Velocity ratio Method written by Rudolph W. Hensel and published by . This book was released on 1951 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculations of the ratios of the velocity increments at test bodies to those at the tunnel walls caused by the solid blocking of these bodies within the walls of a closed rectangular wind tunnel are presented. The boides treated include two-dimensional airfoils; small bodies of revolution; straight, untapered, finite-span wings of varying span; and swept, untapered, finite-span wings of varying span. It is shown that, after wake blocking effects have been removed , the present method furnishes semiempirical blocking corrections for most wind-tunnel models and their components. The test section proportions of the Southern California Cooperative Wind Tunnel at CIT (ratio of height to width equal to 1/square root of 2) are used in the calculations.

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1963
  • ISBN :
  • Pages : 694 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1963 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Advances in Applied Mechanics

Download or read book Advances in Applied Mechanics written by and published by Academic Press. This book was released on 1958-01-01 with total page 471 pages. Available in PDF, EPUB and Kindle. Book excerpt: Advances in Applied Mechanics