Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack
| Author | : Franklin K. Moore |
| Publisher | : |
| Total Pages | : 710 |
| Release | : 1951 |
| ISBN-10 | : STANFORD:36105024831245 |
| ISBN-13 | : |
| Rating | : 4/5 (45 Downloads) |
Book Synopsis Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack by : Franklin K. Moore
Download or read book Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack written by Franklin K. Moore and published by . This book was released on 1951 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: The laminar boundary layer on a circular cone at angle of attack to a supersonic stream is discussed. A perturbation analysis was made to show the influence of a small angle of attack on such boundary layer quantities as skin friction, boundary-layer thickness, viscous lift, drag, and pitching moment.
