Characteristics of the AT-303 hypersonic wind tunnel. Part 1. Velocity Fields |
| |
| Authors: | A M Kharitonov V I Zvegintsev L G Vasenev A D Kuraeva D G Nalivaichenko A V Novikov M A Paikova V F Chirkashenko N V Shakhmatova S I Shpak |
| |
| Institution: | (1) Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia |
| |
| Abstract: | The structure and principle of operation of a new wind tunnel AT-303 with adiabatic compression are described. Results of
systematic investigations are presented in terms of velocity distributions both at the nozzle exit and in the region where
the models are located. The velocity fields are obtained with the use of total pressure probes in the ranges of Mach numbers
from 7.6 to 19.7 and Reynolds numbers per meter Re1 = (0.25−3.64)·107. |
| |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ |
