| dc.contributor.author | Peterson, Carl R. | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Gas Turbine Laboratory | en_US |
| dc.date.accessioned | 2016-10-06T21:22:07Z | |
| dc.date.available | 2016-10-06T21:22:07Z | |
| dc.date.issued | 1958 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/104713 | |
| dc.description | December 1958 | en_US |
| dc.description | This report was originally the authors master's thesis: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1958) | en_US |
| dc.description | Includes bibliographical references | en_US |
| dc.description.abstract | A study of the turbulent boundary layer on an airfoil in a cascade is presented. The major portion of the observations are on the suction surface of the airfoil. The effect of added diffusion across the cascade due to a three-dimensional flow is included. Empirical equations describing the boundary layer in terms of momentum and displacement thickness growth as a function of free-stream diffusion are developed. Shape factor is also related to free-stream diffusion. A reasonable check with an existing separation criterion is observed. An appendix contains a discussion of chord-wise integrating of various boundary layer parameters. | en_US |
| dc.description.sponsorship | Under the sponsorship of: General Electric Company, Allison Division of General Motors Corporation and Westinghouse Electric Corporation | en_US |
| dc.format.extent | [56] leaves in various foliations (some unnumbered) | en_US |
| dc.publisher | [Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958] | en_US |
| dc.relation.ispartofseries | GTL report #49 | en_US |
| dc.subject.lcc | TJ778.M41 G24 no.49 | en_US |
| dc.subject.lcsh | Boundary layer | en_US |
| dc.title | Boundary layer on an airfoil in a cascade | en_US |
| dc.type | Technical Report | en_US |
| dc.identifier.oclc | 14200024 | en_US |
