A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels

Download or Read eBook A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels PDF written by C. J. Schueler and published by . This book was released on 1963 with total page 42 pages. Available in PDF, EPUB and Kindle.
A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels
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Total Pages : 42
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ISBN-10 : UOM:39015104951556
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Book Synopsis A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels by : C. J. Schueler

Book excerpt: Transition Reynolds number measurements on a hollow cylinder in the von Karman Gas Dynamics Facility's 12-inch and 40-inch supersonic tunnels show that the highest transition Reynolds numbers were obtained in the 40-inch tunnel, although the variations with unit Reynolds number were the same at Mach numbers 3 to 5. The influence of nose bluntness in the 40-inch tunnel corresponds closely with the results obtained in the 12-inch tunnel.


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