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Book A Method for the Calculation of External Lift  Moment  and Pressure Drag of Slender Open nose Bodies of Revolution at Supersonic Speeds

Download or read book A Method for the Calculation of External Lift Moment and Pressure Drag of Slender Open nose Bodies of Revolution at Supersonic Speeds written by A. M. Peiser and published by . This book was released on 1944 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1955
  • ISBN :
  • Pages : 22 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 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report   National Advisory Committee for Aeronautics

Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 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   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 1945 with total page 752 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 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NACA Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1945
  • ISBN :
  • Pages : 712 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 1945 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release :
  • ISBN :
  • Pages : 284 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 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 664 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 1949 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Linearized Theory of Steady High Speed Flow

Download or read book Linearized Theory of Steady High Speed Flow written by G. N. Ward and published by Cambridge University Press. This book was released on 2016-02-25 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.

Book Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method

Download or read book Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method written by E. R. G. Eckert and published by . This book was released on 1955 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Memorandum

Download or read book NASA Memorandum written by and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Memorandum

    Book Details:
  • Author : United States. National Aeronautics and Space Administration
  • Publisher :
  • Release : 1959
  • ISBN :
  • Pages : 384 pages

Download or read book NASA Memorandum written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Handbook of Supersonic Aerodynamics

Download or read book Handbook of Supersonic Aerodynamics written by D. Adamson and published by . This book was released on 1961 with total page 366 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Handbook of Supersonic Aerodynamics

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1961 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1949 with total page 412 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book General Theory of Wave drag Reduction for Combinations Employing Quasi cylindrical Bodies with an Application to Swept wing and Body Combinations

Download or read book General Theory of Wave drag Reduction for Combinations Employing Quasi cylindrical Bodies with an Application to Swept wing and Body Combinations written by Jack N. Nielsen and published by . This book was released on 1956 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt: The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with quasi-cylindrical bodies permits the direct calculation of pressure-distribution changes produced by body shape changes. This theory is used to determine the relative magnitued of the wave-drag reduction produced by changes in cylinder cross-sectional area and that produced changes in cross-sectional shape (without change in area). The body distortion is expressed as a Fourier series, and an integral equation is derived for the body shape for minimum drag for each Fourier component. Thus the wave-drag reductions for the various Fourier harmonics are independent and additive.