Zobrazeno 1 - 4
of 4
pro vyhledávání: '"R. W. Whitside"'
Publikováno v:
Shock Waves. 31:419-426
The operation of free-piston-driven reflected shock tunnels has largely observed the rule of thumb that the nozzle throat diameter should not exceed one third the shock-tube diameter. This is intended to ensure drainage does not prematurely terminate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc23bdc18807a4923390959bbf398eea
https://doi.org/10.1007/s00193-021-01017-7
https://doi.org/10.1007/s00193-021-01017-7
Autor:
Wilson Y. K. Chan, Peter A. Jacobs, Michael K. Smart, David Gildfind, Tamara Sopek, R. W. Whitside
Publikováno v:
Shock Waves. 31:541-550
Nitrogen is proposed as a suitable driver gas candidate for the operation of free-piston-driven shock tunnels at low total enthalpies. When compressed adiabatically, nitrogen has a lower speed of sound than the commonly used driver gases, e.g., argon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3d9aeb1b52b0659c15b82ba181868b29
https://doi.org/10.1007/s00193-021-01002-0
https://doi.org/10.1007/s00193-021-01002-0
Autor:
R. W. Whitside, Michael K. Smart
Publikováno v:
23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Experiments with a scramjet engine for a planned Mach 5–10 access-to-space vehicle have been undertaken in the T4 reflected shock tunnel at low Mach number conditions. The 3D scramjet flowpath is designed to integrate with a conical vehicle and inv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02a366f7febe19c8e0cf86548bb9d568
https://doi.org/10.2514/6.2020-2435
https://doi.org/10.2514/6.2020-2435
Publikováno v:
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::206d84f75f95ee44c632dae3d36a30e0
https://doi.org/10.3850/978-981-11-2730-4_0305-cd
https://doi.org/10.3850/978-981-11-2730-4_0305-cd