Zobrazeno 1 - 10
of 27
pro vyhledávání: '"W. K. Van Moorhem"'
Autor:
W. K. Van Moorhem, Alison B. Flatau
Publikováno v:
Journal of Propulsion and Power. 19:287-296
Results are presented from a cold-flow investigation of acoustic responses driven by flow through two annular baffles in a cylindrical cavity, having (approximately) closed-closed end conditions. The interaction of the flow with cavity acoustic reson
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d556c5dd40d3fccf986e94221022259
https://doi.org/10.2514/2.6110
https://doi.org/10.2514/2.6110
Autor:
Joseph Majdalani, W. K. Van Moorhem
Publikováno v:
Journal of Propulsion and Power. 13:186-193
The acoustic boundary-layer structure is investigated in a cylindrical tube where steady sidewall injection is imposed upon an oscillatory e ow. Culick’ s steady, rotational, and inviscid solution is assumed for the mean e ow. The time-dependent ve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78db2c9d5ffb6caf49df8fb0d6101ce9
https://doi.org/10.2514/2.5168
https://doi.org/10.2514/2.5168
Analytical and Experimental Analysis of a Self-Compensating Dynamic Balancer in a Rotating Mechanism
Autor:
Jongkil Lee, W. K. Van Moorhem
Publikováno v:
Journal of Dynamic Systems, Measurement, and Control. 118:468-475
A theoretical and experimental approach was used to investigate the motion and effectiveness of a Self-Compensating Dynamic Balancer (SCDB). This is a device intended to minimize the effects of rotor imbalance and vibratory forces on a rotating syste
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6faca251018a7efd9d202e2e28dadb7f
https://doi.org/10.1115/1.2801169
https://doi.org/10.1115/1.2801169
Autor:
Mohammad Nasiri, W. K. Van Moorhem
Publikováno v:
International Communications in Heat and Mass Transfer. 23:613-622
Heat transfer in an oscillating flow at high acoustic Reynolds number has been investigated using the mass-transfer analogy. Subliming naphthalene has been used in the experiments. In these experiments the acoustic Reynolds number was varied over a r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2cb082b3ad4b86b3442a87047fd6508
https://doi.org/10.1016/0735-1933(96)00044-9
https://doi.org/10.1016/0735-1933(96)00044-9
Publikováno v:
Journal of Propulsion and Power. 7:692-699
An investigation has been conducted of the velocity coupling phenomenon reported in acoustically unstable solid-propellant rocket motors. An innovative simulation facility has been built using solid carbon dioxide as the simulated propellant. Acousti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::820b0f5fd814e8f55d8d189f2608c814
https://doi.org/10.2514/3.23381
https://doi.org/10.2514/3.23381
Publikováno v:
Journal of Vibration and Acoustics. 112:550-555
An investigation has been conducted of the velocity coupling phenomenon reported in acoustically unstable solid propellant rocket motors. An innovative simulation facility has been built using solid carbon dioxide as the simulated propellant. The use
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a455ecaf015b67eb36e0db6c16e55414
https://doi.org/10.1115/1.2930141
https://doi.org/10.1115/1.2930141
Autor:
Joseph Majdalani, W. K. Van Moorhem
Publikováno v:
37th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4fda8b837888d57fbf4e3406943680d
https://doi.org/10.2514/6.2001-3589
https://doi.org/10.2514/6.2001-3589
Publikováno v:
7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d4cbe1f64e04b12e759e2697f8522b7
https://doi.org/10.2514/6.1998-2582
https://doi.org/10.2514/6.1998-2582
Publikováno v:
29th AIAA, Fluid Dynamics Conference.
In this work, the onset of turbulence inside a rectangular chamber is investigated, with and without side-wall injection, in the presence of an oscillatory pressure gradient. Three techniques are used to define the transition from laminar to turbulen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5e6df1176db7ab5fdcc337dccfa442b
https://doi.org/10.2514/6.1998-2808
https://doi.org/10.2514/6.1998-2808
Publikováno v:
28th Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43221821d8166e6b5fdf7096430af491
https://doi.org/10.2514/6.1990-557
https://doi.org/10.2514/6.1990-557