Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Cooled Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1974 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Cooled Turbine Vanes Trailing edge ejection film cooling and transpiration cooling written by Goldman, Louis J. and published by . This book was released on 1975 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1976 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Cooled Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1975 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by Louis J. Goldman and published by . This book was released on 1975 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by Goldman, Louis J. and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by McLallin, Kerry L. and published by . This book was released on 1976 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by Kerry L. McLallin and published by . This book was released on 1976 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes Pressure surface trailing edge ejection and split trailing edge ejection written by Goldman, Louis J. and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Cooled Turbine Vanes Trailing edge ejection film cooling and transpiration cooling written by Goldman, Louis J. and published by . This book was released on 1975 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Cooled Turbine Vanes written by Goldman, Louis J. and published by . This book was released on 1974 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cold air Annular cascade Investigation of Aerodynamic Performance of Core engine cooled Turbine Vanes written by Kerry L. McLallin and published by . This book was released on 1976 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Performance of a Fully Film Cooled Core Turbine Vane Tested with Cold Air in a Two dimensional Cascade written by Roy G. Stabe and published by . This book was released on 1975 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic performance of a fully film cooled core turbine vane was investigated experimentally in a two-dimensional cascade of 10 vanes. Three of the 10 vanes were cooled; the others were solid (uncooled) vanes. Cold air was used for both the primary and coolant flows. The cascade test covered a range of pressure ratios corresponding to ideal exit critical velocity ratios of 0.6 to 0.95 and a range of coolant flow rates to 7.5 percent of the primary flow. The coolant flow was varied by changing the coolant supply pressure. The principal measurements were cross-channel surveys of exit total pressure, static pressure, and flow angle. The results presented include exit survey data and overall performance in terms of loss, flow angle, and weight flow for the range of exit velocity ratios and coolant flows investigated. The performance of the cooled vane is compared with the performance of an uncooled vane of the same profile and also with the performance obtained with a single cooled vane in the 10-vane cascade.

Download or read book Effect of Cooling hole Geometry on Aerodynamic Performance of a Film cooled Turbine Vane Tested with Cold Air in a Two dimensional Cascade written by John F. Kline and published by . This book was released on 1978 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid vane Performance and Facility Description written by Louis J. Goldman and published by . This book was released on 1975 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1981 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1976 with total page 1072 pages. Available in PDF, EPUB and Kindle. Book excerpt: