Tangential Velocity Measurements
Author | : Bruce C. Murray |
Publisher | : |
Total Pages | : 36 |
Release | : 1960 |
Genre | : Contact transformations |
ISBN | : |
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Author | : Bruce C. Murray |
Publisher | : |
Total Pages | : 36 |
Release | : 1960 |
Genre | : Contact transformations |
ISBN | : |
Author | : Bruce C. Murray |
Publisher | : |
Total Pages | : 1 |
Release | : 1960 |
Genre | : Contact transformations |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 26 |
Release | : 2002 |
Genre | : |
ISBN | : |
An Interferometric Moving Target Indicator radar can be used to measure the tangential velocity component of a moving target. Multiple baselines, along with the conventional radial velocity measurement, allow estimating the true 3-D velocity vector of a target.
Author | : Daniel L. Bulzan |
Publisher | : |
Total Pages | : 20 |
Release | : 1996 |
Genre | : |
ISBN | : |
Author | : Woon Don Chai |
Publisher | : |
Total Pages | : 226 |
Release | : 1988 |
Genre | : |
ISBN | : |
Author | : Bahram Dabir |
Publisher | : |
Total Pages | : 544 |
Release | : 1983 |
Genre | : Fluid mechanics |
ISBN | : |
Author | : Michael Robert Hime |
Publisher | : |
Total Pages | : 254 |
Release | : 1998 |
Genre | : |
ISBN | : |
Author | : John Raymond Haines |
Publisher | : |
Total Pages | : 248 |
Release | : 1980 |
Genre | : Fluid mechanics |
ISBN | : |
Author | : William M. Stanley |
Publisher | : |
Total Pages | : 68 |
Release | : 1968 |
Genre | : |
ISBN | : |
An experimental investigation was conducted to examine the flow field within the chamber of a spinning, cold flow rocket motor and to determine the effects of the interaction of this swirling flow with the decreasing area of a converging nozzle. The investigation was divided into two phases: (a) the measurement of the static pressure and velocity profiles within the chamber of the cold flow motor with a five-port impact tube probe and (b) the measurement of the effect of the swirling flow-nozzle interaction on the mass flow rate through the nozzle. The static pressure and velocity profiles were measured at two axial locations within the chamber of a simulated end-burning rocket motor for rotational speeds of 1000, 3000 and 5000 rpm. The measured axial and tangential velocity profiles ere compared with the predicted profiles, which were based upon a solid-body vortex with a uniform axial velocity. (Author).
Author | : David S. King |
Publisher | : |
Total Pages | : 9 |
Release | : 1982 |
Genre | : |
ISBN | : |
The tangential velocity distribution of ground state NO (J' = 9 1/2, E(rot)=165/cm) thermally desorbed from Ru(001) under ultra-high vacuum conditions was measured by laser excited fluorescence Doppler spectroscopy. The measured Doppler profile was Gaussian in nature, characterized by a temperature T = 235 + or - 45 K significantly lower than the surface temperature at the desorption peak of 455 K.