Lecture Series "Boundary Layer Theory.": Laminar flows
Author | : Hermann Schlichting |
Publisher | : |
Total Pages | : 180 |
Release | : 1949 |
Genre | : Boundary layer |
ISBN | : |
Download Lecture Series Boundary Layer Theory Part I full books in PDF, epub, and Kindle. Read online free Lecture Series Boundary Layer Theory Part I ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Hermann Schlichting |
Publisher | : |
Total Pages | : 180 |
Release | : 1949 |
Genre | : Boundary layer |
ISBN | : |
Author | : Hermann Schlichting |
Publisher | : |
Total Pages | : 148 |
Release | : 1949 |
Genre | : Boundary layer |
ISBN | : |
Author | : Hermann Schlichting (Deceased) |
Publisher | : Springer |
Total Pages | : 814 |
Release | : 2016-10-04 |
Genre | : Technology & Engineering |
ISBN | : 366252919X |
This new edition of the near-legendary textbook by Schlichting and revised by Gersten presents a comprehensive overview of boundary-layer theory and its application to all areas of fluid mechanics, with particular emphasis on the flow past bodies (e.g. aircraft aerodynamics). The new edition features an updated reference list and over 100 additional changes throughout the book, reflecting the latest advances on the subject.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 616 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1026 |
Release | : 1956 |
Genre | : Aeronautics |
ISBN | : |
Author | : Maurice Tucker |
Publisher | : |
Total Pages | : 686 |
Release | : 1951 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
An analytical method is presented for obtaining turbulent temperature recovery factors for a thermally insulated surface in supersonic flow. The method is an extension of Squire's analysis for incompressible flow. The boundary layer velocity profile is represented by a power law and a similarity is postulated for squared-velocity the static-temperature-difference profiles.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 612 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Chiefly translations from foreign aeronautical journals.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 574 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Chiefly translations from foreign aeronautical journals.