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| Author | : |
| Publisher | : |
| Total Pages | : 37 |
| Release | : 1959 |
| Genre | : Boundary layer |
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| Author | : Ivan E. Beckwith |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1959 |
| Genre | : Boundary layer |
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| Author | : |
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| Total Pages | : 1 |
| Release | : 1960 |
| Genre | : |
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| Author | : |
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| Total Pages | : 1878 |
| Release | : 1961 |
| Genre | : Government publications |
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| Author | : George M. Low |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1955 |
| Genre | : Aerodynamic heating |
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A solution of the equations of the compressible laminar boundary layer including the effects of transpiration cooling is presented. The analysis applies to the flow over an isothermal porous plate with a velocity of fluid injection proportional to the reciprocal of the square root of the distance from the leading edge.
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| Total Pages | : 244 |
| Release | : 1962 |
| Genre | : |
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| Author | : Library of Congress. Science and Technology Division |
| Publisher | : |
| Total Pages | : 244 |
| Release | : 1962 |
| Genre | : Aeronautics |
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| Author | : Eli Reshotko |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1957 |
| Genre | : Aerodynamic heating |
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The equations for development of the compressible laminar boundary layer over a yawed infinite cylinder are presented. For compressible flow with a pressure gradient the chordwise and spanwise flows are not independent. By use of the Stewartson transformation and a linear viscosity-temperature relation, a set of three simultaneous ordinary differential equations is obtained in a form yielding similar solutions. These equations are solved for stagnation-line flow for surface temperatures from zero to twice the free-stream stagnation temperature and for a wide range of yaw angle and free-stream Mach number.
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| Total Pages | : 118 |
| Release | : 1971 |
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| Author | : |
| Publisher | : |
| Total Pages | : 33 |
| Release | : 1959 |
| Genre | : Cooling |
| ISBN | : |
