Description

Book Synopsis

Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes.

Originally published in 1960.

The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its foundi

Table of Contents
*Frontmatter, pg. i*Preface, pg. vi*Contents, pg. 1*1. Introduction, pg. 3*2. Subsonic Flows, pg. 10*3. Supersonic Two-Dimensional Airfoil Theory: Surface Pressures, pg. 31*4. Supersonic Two-dimensional Airfoil Theory: Complete Flow Pattern, pg. 54*5. Supersonic Two-dimensional Airfoil Theory: Influence of a Blunt Leading Edge, pg. 74*6. Supersonic Projectile Theory: Complete Flow Pattern, pg. 83*7. Supersonic Projectile Theory: Surface Pressures, pg. 109*8. Supersonic Three-dimensional Wing Theory, pg. 135*9. Cited References, pg. 145

Higher Approximations in Aerodynamic Theory

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    Order before 4pm tomorrow for delivery by Wed 17 Jun 2026.

    A Paperback by M. J. Lighthill

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      View other formats and editions of Higher Approximations in Aerodynamic Theory by M. J. Lighthill

      Publisher: Princeton University Press
      Publication Date: 2/16/2016 12:00:00 AM
      ISBN13: 9780691626017, 978-0691626017
      ISBN10: 0691626014

      Description

      Book Synopsis

      Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes.

      Originally published in 1960.

      The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its foundi

      Table of Contents
      *Frontmatter, pg. i*Preface, pg. vi*Contents, pg. 1*1. Introduction, pg. 3*2. Subsonic Flows, pg. 10*3. Supersonic Two-Dimensional Airfoil Theory: Surface Pressures, pg. 31*4. Supersonic Two-dimensional Airfoil Theory: Complete Flow Pattern, pg. 54*5. Supersonic Two-dimensional Airfoil Theory: Influence of a Blunt Leading Edge, pg. 74*6. Supersonic Projectile Theory: Complete Flow Pattern, pg. 83*7. Supersonic Projectile Theory: Surface Pressures, pg. 109*8. Supersonic Three-dimensional Wing Theory, pg. 135*9. Cited References, pg. 145

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