Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781729285206
Total Pages : 50 pages
Book Rating : 4.2/5 (852 download)
Book Synopsis Hydrogen Film Cooling with Incident and Swept-Shock Interactions in a Mach 6.4 Nitrogen Free Stream by : National Aeronautics and Space Adm Nasa
Download or read book Hydrogen Film Cooling with Incident and Swept-Shock Interactions in a Mach 6.4 Nitrogen Free Stream written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-10-26 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effectiveness of slot film cooling of a flat plate in a Mach 6.4 flow with and without incident and swept oblique shock interactions was experimentally investigated. Hydrogen was the primary coolant gas, although some tests were conducted using helium as the coolant. Tests were conducted in the Calspan 48-Inch Shock Tunnel with a nitrogen flow field to preclude combustion of the hydrogen coolant gas. A two-dimensional highly instrumented model developed in a previous test series was used. Parameters investigated included coolant mass flow rate, coolant gas, local free-stream Reynolds number, incident oblique shock strength, and a swept oblique shock. Both gases were highly effective coolants in undisturbed flow; however, both incident and swept shocks degraded that effectiveness. Olsen, George C. and Nowak, Robert J. Langley Research Center RTOP 506-43-31-03...