Experimental Study Of Stability And Transition Of Hypersonic Boundary Layer Around Blunted Cone
Download Experimental Study Of Stability And Transition Of Hypersonic Boundary Layer Around Blunted Cone PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Experimental Study Of Stability And Transition Of Hypersonic Boundary Layer Around Blunted Cone book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
Experimental Study of Stability and Transition of Hypersonic Boundary Layer Around Blunted Cone
The objective of this project is to basic research of stability and transition of hypersonic boundary layer around blunted cone. Next results is obtained: -experimental data on the position of the laminar-turbulent transition in the boundary layer of a cone with different nose bluntness for Mach 6; -experimental data on the characteristics of natural disturbances in the hypersonic boundary layer of a blunted cone for Mach 6; -experimental data on the evolution of artificial disturbances, excited in the hypersonic boundary layer on a blunted cone for Mach 6. Acquired experimental data could be used for validation of numerical techniques. Using of obtained data will help to more accurate prediction of laminar-turbulent transition location and thereby heat fluxes on hypersonic vehicles.