Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Elizabeth H. Weidner"'
Autor:
Elizabeth H. Weidner, R. C. Rogers
Publikováno v:
Journal of Propulsion and Power. 9:127-133
A numerical simulation of the temporally developing flow through a generic scramjet combustor duct is presented for stagnation conditions typical of flight at Mach 13. The particular focus is to examine the startup transients and to determine the tim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::862933184850891633b259ddac1b9ef1
https://doi.org/10.2514/3.11494
https://doi.org/10.2514/3.11494
Publikováno v:
Journal of Propulsion and Power. 8:890-899
The establishment of a quasi-steady flow in a generic scramjet combustor was studied for the case of a time varying inflow to the combustor. Such transient flow is characteristic of the reflected shock tunnel and expansion tube test facilities. Sever
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd175e67f713c6b73ef22c964214fe0e
https://doi.org/10.2514/3.23566
https://doi.org/10.2514/3.23566
Publikováno v:
25th Plasmadynamics and Lasers Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ca3747305c609451527b77614a02cc1
https://doi.org/10.2514/6.1994-2518
https://doi.org/10.2514/6.1994-2518
Publikováno v:
29th Aerospace Sciences Meeting.
A numerical simulation of the temporally developing flow through a generic scramjet combustor duct is presented for stagnation conditions typical of flight at Mach 13 as produced by a shock tunnel pulse facility. The particular focus is to examine th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e964fc1b7eb5e96849b22a34297843d
https://doi.org/10.2514/6.1991-229
https://doi.org/10.2514/6.1991-229
Publikováno v:
AIAA Journal. 20:1182-1187
A computer program has been developed to analyze the turbulent reacting flow field in a two-dimensional scramjet engine configuration. The program numerically solves the full two-dimensional Navier-Stokes and species equations in the engine inlet and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce5c90714f979f64a56f1b9b890c62bc
https://doi.org/10.2514/3.51178
https://doi.org/10.2514/3.51178
Publikováno v:
AIAA Journal. 20:1426-1431
A parametric study of staged (multiple) perpendicular fuel injector configurations has been conducted using a computer code that solves the two-dimensional elliptic Navier-Stokes equations. The program computes the turbulent mixing and reaction of hy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3cc221d51b53523ac9fbd120cff91ca
https://doi.org/10.2514/3.51202
https://doi.org/10.2514/3.51202
Publikováno v:
24th Joint Propulsion Conference.
The supersonic high enthalpy flow from a shock tunnel facility flowing through a two-dimensional duct simulating a combustor has been computed for two test conditions for both steady and transient inflow. The nominal test conditions had stagnation en
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec712b19d77386e0667f0bd074460dcb
https://doi.org/10.2514/6.1988-3261
https://doi.org/10.2514/6.1988-3261
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