Laminar Boundary Layer On A Circular Cone In Supersonic Flow At A Small Angle Of Attack
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Author | : Franklin K. Moore |
Publisher | : |
Total Pages | : 710 |
Release | : 1951 |
Genre | : Angle of attack (Aerodynamics) |
ISBN | : |
Download Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack Book in PDF, Epub and Kindle
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.
Author | : Cornell University. Graduate School of Aeronautical Engineering |
Publisher | : |
Total Pages | : |
Release | : 1956 |
Genre | : |
ISBN | : |
Download Laminar Boundary Layer on a Spinning Circular Cone in Supersonic Flow at a Small Angle of Attack Book in PDF, Epub and Kindle
Author | : Martin Fiebig |
Publisher | : |
Total Pages | : 0 |
Release | : 1956 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Laminar Boundary Layer on a Spinning Circular Cone in Supersonic Flow at a Small Angle of Attack Book in PDF, Epub and Kindle
Author | : Willis H. Braun |
Publisher | : |
Total Pages | : 24 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Turbulent Boundary Layer on a Yawed Cone in a Supersonic Stream Book in PDF, Epub and Kindle
Author | : Willis H. Braun |
Publisher | : |
Total Pages | : 28 |
Release | : 1959 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Turbulent Boundary Layer on a Yawed Cone in a Supersonic Stream Book in PDF, Epub and Kindle
The momentum integral equations are derived for the boundary layer on an arbitrary curved surface, using a streamline coordinate system. Computations of the turbulent boundary layer on a slightly yawed cone are made for a Prandtl number of 0.729, wall to free-stream temperature ratios of 1/2, 1, and 2, and Mach numbers from 1 to 4. Deflection of the fluid in the boundary layer from outer stream direction, local friction coefficient, displacement surface, lift coefficient, and pitching-moment coefficient are presented.
Author | : Arloe Wesley Mayne (Jr.) |
Publisher | : |
Total Pages | : 114 |
Release | : 1972 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1216 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Author | : Franklin K. Moore |
Publisher | : |
Total Pages | : 13 |
Release | : 1953 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack Book in PDF, Epub and Kindle
The laminar-boundary-layer flow about a cone at large angles of attack to a supersonic stream has been analyzed in the plane of symmetry. At the bottom of the cone, velocity profiles were obtained showing the expected tendency of the boundary layer to become thinner on the under side of the cone as the angle of attack is increased. At the top of the cone, the analysis failed to yield unique solutions, except for small angles of attack. Beyond a certain critical angle of attack, boundary-layer flow does not exist in the plane of symmetry, thus indicating separation.
Author | : Joseph L. Sims |
Publisher | : |
Total Pages | : 440 |
Release | : 1964 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 620 |
Release | : 1974 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, Epub and Kindle