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Book Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release :
  • ISBN :
  • Pages : 412 pages

Download or read book Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 412 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wartime Report

Download or read book Wartime Report written by and published by . This book was released on with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Report

    Book Details:
  • Author : Aeronautical Research Council (Great Britain)
  • Publisher :
  • Release : 1960
  • ISBN :
  • Pages : 728 pages

Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1960 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.

Book NACA Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release :
  • ISBN :
  • Pages : 606 pages

Download or read book NACA Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Lifting surface theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces

Download or read book Lifting surface theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces written by Robert S. Swanson and published by . This book was released on 1945 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation was made by lifting-surface theory of a thin elliptic wing of aspect ratio 6 in a steady roll by means of the electromagnetic-analogy method. From the results, aspect-ratio corrections for the damping in roll and aileron hinge moments for a wing in steady roll were obtained that are considerably more accurate than those given by lifting-line theory. First-order effects of compressibility were included in the computations. The results obtained by lifting-surface theory indicate that the damping in roll for a wing of aspect ratio 6 is 13 percent less than that given by lifting-line theory and 5 percent less than that given by lifting-line theory with the edge-velocity correction derived by Robert T. Jones applied. The results are extended to wings of other aspect ratios.

Book Technical Note

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1947
  • ISBN :
  • Pages : 494 pages

Download or read book Technical Note written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 494 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Research Abstracts

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1951
  • ISBN :
  • Pages : 568 pages

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 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 1947 with total page 1070 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of the Royal Aeronautical Society

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1953 with total page 954 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation of Ailerons on a Low drag Airfoil

Download or read book Wind tunnel Investigation of Ailerons on a Low drag Airfoil written by Robert M. Crane and published by . This book was released on 1944 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Ames Aeronautical Laboratory 7- by 10-foot wind tunnel of the effects of a trailing edge of a 0.20-chord plain sealed aileron on an NACA 66,2-216 (a = 0.6) airfoil.

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 446 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 1943 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt: