Zobrazeno 1 - 10
of 14
pro vyhledávání: '"W. C. Elrod"'
Autor:
Mark R. Goodell, W. C. Elrod
Publikováno v:
Journal of Spacecraft and Rockets. 32:411-416
The utility of suborbital launch trajectories to increase the payload capacity for a hypersonic-lifting-body launch vehicle was investigated. This type of trajectory involves deployment of a payload and booster motor from the launch vehicle at suborb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9be74d6e5fa3ffec4dd6d40f444e3cee
https://doi.org/10.2514/3.26630
https://doi.org/10.2514/3.26630
Publikováno v:
Journal of Propulsion and Power. 9:293-300
Trailing-edge crenulations have been shown to enhance velocity recovery (wake dissipation) and to decrease total pressure losses in the blade wakes downstream of a low-aspect ratio linear compressor cascade. A new study was performed to determine the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12205bc0541c908b497cc054631db149
https://doi.org/10.2514/3.23621
https://doi.org/10.2514/3.23621
Publikováno v:
Journal of Turbomachinery. 113:479-483
The mechanisms influencing film cooling effectiveness on a flat plate in high free-stream turbulence using a single row of 30 deg slant-hole injectors are examined. The primary area of focus is the area within 40 diameters downstream of injection. Of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef18accfd2d879faaee5bc99a81904e2
https://doi.org/10.1115/1.2927899
https://doi.org/10.1115/1.2927899
Publikováno v:
26th Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c8dddd9257d3e07f638b7182d7f01e05
https://doi.org/10.2514/6.1990-2264
https://doi.org/10.2514/6.1990-2264
Publikováno v:
26th Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::deac8a68cfe7a4d70ec5b1c01cd3681a
https://doi.org/10.2514/6.1990-2412
https://doi.org/10.2514/6.1990-2412
Publikováno v:
Volume 1: Turbomachinery.
The effects of surface roughness, freestream turbulence, and incidence angle on the performance of a two-dimensional compressor cascade were investigated. The test section consisted of seven NACA 65-A506 airfoils arranged in a linear cascade. Four di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48cc00f5d08f9f7581d013686ec802f8
https://doi.org/10.1115/90-gt-208
https://doi.org/10.1115/90-gt-208
Publikováno v:
Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; General.
Trailing edge crenulations offer one possible way of energizing the trailing edge wakes from a gas turbine engine compressor blade by creating small vortices as a result of the pressure differential between the suction surface and pressure surface. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e39ecd18747a58d780043c4f23c04be2
https://doi.org/10.1115/90-gt-218
https://doi.org/10.1115/90-gt-218
Publikováno v:
Journal of Turbomachinery. 111:78-86
The effects of the longitudinal turbulence intensity parameter of free-stream turbulence (FST) on heat transfer were studied using the aggressive flow characteristics of a circular tangential wall jet over a constant heat flux surface. Profile measur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::270817ee4903c7081631efb1ca851d58
https://doi.org/10.1115/1.3262240
https://doi.org/10.1115/1.3262240
Publikováno v:
Journal of Heat Transfer. 89:235-242
Data are presented for natural and forced convection heat transfer from the outside of a single 3/4-in-dia tube to saturated water in the pressure range from 535 to 1550 psia. Nonboiling and nucleate boiling at low heat flux are considered for vertic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4cb988496a64ae87cb4e62fbaac34d56
https://doi.org/10.1115/1.3614368
https://doi.org/10.1115/1.3614368
Publikováno v:
10th Aerodynamic Testing Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba36ac7422527cbd915a8bfd2984befe
https://doi.org/10.2514/6.1978-820
https://doi.org/10.2514/6.1978-820