Laminar Heat Transfer And Pressure Measurements At A Mach Number Of 6 On A Sharp And Blunt 15 Half Angle Cones At Angles Of Attack Up To 90
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Author | : Raul Jorge Conti |
Publisher | : |
Total Pages | : 38 |
Release | : 1961 |
Genre | : Heat |
ISBN | : |
Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.
Author | : |
Publisher | : |
Total Pages | : 1878 |
Release | : 1961 |
Genre | : Government publications |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1250 |
Release | : 1979 |
Genre | : United States |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 528 |
Release | : 1973 |
Genre | : Mechanics, Applied |
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Author | : |
Publisher | : |
Total Pages | : 994 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : Dennis M. Bushnell |
Publisher | : |
Total Pages | : 40 |
Release | : 1968 |
Genre | : Aerodynamics |
ISBN | : |
Author | : California Institute of Technology. Graduate Aeronautical Laboratories |
Publisher | : |
Total Pages | : 166 |
Release | : |
Genre | : Aerodynamics, Hypersonic |
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Author | : Sandia Corporation |
Publisher | : |
Total Pages | : 596 |
Release | : 1965 |
Genre | : Aerodynamics |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1248 |
Release | : 1961 |
Genre | : Government publications |
ISBN | : |
Author | : Jim A. Penland |
Publisher | : |
Total Pages | : 48 |
Release | : 1964 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |