Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Some Finite Difference Solutions Of Laminar Compressible Boundary Layer Showing Effects Of Upstream Transpiration Cooling With List Of References PDF full book. Access full book title Some Finite Difference Solutions Of Laminar Compressible Boundary Layer Showing Effects Of Upstream Transpiration Cooling With List Of References.
| Author | : |
| Publisher | : |
| Total Pages | : 33 |
| Release | : 1959 |
| Genre | : Cooling |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2106 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
| Author | : Donald Charles Baxter |
| Publisher | : |
| Total Pages | : 620 |
| Release | : 1957 |
| Genre | : Boundary layer |
| ISBN | : |
| Author | : George M. Low |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1955 |
| Genre | : Aerodynamic heating |
| ISBN | : |
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.
| Author | : Stanford University. Division of Engineering Mechanics |
| Publisher | : |
| Total Pages | : 284 |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
| Author | : John T. Howe |
| Publisher | : |
| Total Pages | : 80 |
| Release | : 1959 |
| Genre | : |
| ISBN | : |
| Author | : Stanford University. Division of Engineering Mechanics |
| Publisher | : |
| Total Pages | : 58 |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
| Author | : Stanford University. Division of Engineering Mechanics |
| Publisher | : |
| Total Pages | : 96 |
| Release | : 1956 |
| Genre | : |
| ISBN | : |
| Author | : Er-Yung Yu |
| Publisher | : |
| Total Pages | : 174 |
| Release | : 1960 |
| Genre | : Boundary layer |
| ISBN | : |
| Author | : Jay M. Solomon |
| Publisher | : |
| Total Pages | : 130 |
| Release | : 1967 |
| Genre | : Laminar boundary layer |
| ISBN | : |
An approximate momentum integral solution for the compressible axisymmetrix laminar boundary layer when transverse curvature effects are important is presented. Both finite and infinite inviscid Mach numbers are considered. Detailed comparisons with exact asymptotic solutions are given. The method is found, in many instances, to agree to leading order with the exact solutions as the transverse curvature becomes very large--a property that none of the existing approximate solutions for compressible flow possess. Some example calculations for a cone in supersonic and hypersonic flow are presented. Also, the method is applied to the hypersonic self-induced pressure problem for a cone. (Author).
