Investigation of the Flow Through a Single-stage Two-dimensional Nozzle in the Langley 11-inch Hypersonic Tunnel PDF Download
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Author: Charles H. McLellan Publisher: ISBN: Category : Air flow Languages : en Pages : 30
Book Description
The flow through a two-dimensional, 10.5- by 10-inch nozzle with a design Mach number of 7.08 was investigated. The nozzle was mounted in an intermittant type of tunnel and tested with stagnation conditions of 25 atmospheres and 1210 degrees R. The flow was reasonably uniform in a region approximately 5 inches square in the center of the test section. The Mach number in this region was about 6.86.
Author: Charles H. McLellan Publisher: ISBN: Category : Air flow Languages : en Pages : 30
Book Description
The flow through a two-dimensional, 10.5- by 10-inch nozzle with a design Mach number of 7.08 was investigated. The nozzle was mounted in an intermittant type of tunnel and tested with stagnation conditions of 25 atmospheres and 1210 degrees R. The flow was reasonably uniform in a region approximately 5 inches square in the center of the test section. The Mach number in this region was about 6.86.
Author: A. G. Eubanks Publisher: ISBN: Category : Cobalt oxides Languages : en Pages : 672
Book Description
A series of vitreous coatings of the same basic composition, but with cobalt-oxide contents varying from O to 6.4 percent by weight, fired on ingot iron in atmospheres consisting of various oxygen-nitrogen mixtures. The effect of the oxygen content of the atmosphere on adherence was determined by subjecting each specimen to the American Society for Testing Materials adherence test, and the effect of interface roughness was estimated from examination of metallographic sections.
Author: Charles H. McLellan
Author: Charles H. McLellan
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
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Author: 
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Author: A. G. Eubanks